AIAA-2002-4925 Pursuit Display Review and Extension to a Civil Tilt Rotor Flight Director (Englisch)
- Neue Suche nach: Hardy, G.
- Neue Suche nach: AIAA
- Neue Suche nach: Hardy, G.
- Neue Suche nach: AIAA
In:
Guidance, navigation and control
;
1779-1788
;
2002
-
ISBN:
- Aufsatz (Konferenz) / Print
-
Titel:AIAA-2002-4925 Pursuit Display Review and Extension to a Civil Tilt Rotor Flight Director
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Beteiligte:
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Kongress:Conference, Guidance, navigation and control ; 2002 ; Monterey, CA
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Erschienen in:Guidance, navigation and control ; 1779-1788PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 3 ; 1779-1788
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Verlag:
- Neue Suche nach: AIAA
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Erscheinungsdatum:01.01.2002
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Format / Umfang:10 pages
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ISBN:
-
Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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AIAA-2002-4438 Adaptive Actuator Failure Compensation Designs for a Linearized Aircraft Longitudinal ModelTao, G. / Joshi, S. / Chen, S. / AIAA et al. | 2002
- 12
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AIAA-2002-4439 Adaptive Flight Control for an Autonomous Unmanned HelicopterJohnson, E. / Kannan, S. / AIAA et al. | 2002
- 23
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AIAA-2002-4440 Nonlinear Adaptive Flight Path and Speed Control Using Energy PrinciplesRysdyk, R. / Agarwal, R. / AIAA et al. | 2002
- 34
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AIAA-2002-4441 Flight Evaluation of Adaptive High-Bandwidth Control Methods for Unmanned HelicoptersCorban, J. / Calise, A. / Prasad, J. / Hur, J. / Kim, N. / AIAA et al. | 2002
- 44
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AIAA-2002-4442 Output Feedback Form and Adaptive Control of a Nonlinear Aeroelastic SystemSingh, S. / Wang, L. / AIAA et al. | 2002
- 55
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AIAA-2002-4443 Traffic Complexity Based Conflict ResolutionVisser, H. / Versteegt, H. / AIAA et al. | 2002
- 66
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AIAA-2002-4444 Aircraft Conflict Resolution with an Arrival Time ConstraintBilimoria, K. / Lee, H. / AIAA et al. | 2002
- 77
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AIAA-2002-4445 Conflict Detection and Resolution with Traffic Flow ConstraintsMueller, T. / Schleicher, D. / Bilimoria, K. / AIAA et al. | 2002
- 88
-
AIAA-2002-4446 Development of a Prototype Airborne Conflict Detection and Resolution Simulation CapabilityMondoloni, S. / Palmer, M. / Wing, D. / AIAA et al. | 2002
- 99
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AIAA-2002-4447 Problem Analysis, Resolution and Ranking (PARR) Initial Functional Performance AssessmentKirk, D. / Heagy, W. / Love, W. / Rozen, N. / AIAA et al. | 2002
- 110
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AIAA-2002-4448 A Method of Separation Assurance for Instrument Flight Procedures at Non-RADAR AirportsConway, S. / Consiglio, M. / AIAA et al. | 2002
- 121
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AIAA-2002-4449 Reliable Aircraft Flight Control Using Static Output-FeedbackWang, J. / Yang, G. / Liao, F. / AIAA et al. | 2002
- 130
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AIAA-2002-4450 Designing Robust Large Envelope Flight Controllers for High-Performance AircraftBlue, P. / Odenthal, D. / Muhler, M. / AIAA et al. | 2002
- 139
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AIAA-2002-4451 Flight-Path Angle Control via Neuro-Adaptive BacksteppingSharma, M. / AIAA et al. | 2002
- 147
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AIAA-2002-4452 Model Following Reconfigurable Flight Control System Design Using Direct Adaptive SchemeKim, Y. / Lee, K. / Kim, K. / AIAA et al. | 2002
- 154
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AIAA-2002-4453 A Decentralized Scheme for Autonomous Compensation of Multiple Simultaneous Flight-Critical FailuresBoskovic, J. / Mehra, R. / AIAA et al. | 2002
- 165
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AIAA-2002-4454 An Automated Method to Compute Orbital Re-Entry Trajectories with Heating ConstraintsZimmerman, C. / Dukeman, G. / Hanson, J. / AIAA et al. | 2002
- 174
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AIAA-2002-4455 On-Board Generation of Three-Dimensional Constrained Entry TrajectoriesLu, P. / Shen, Z. / AIAA et al. | 2002
- 190
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AIAA-2002-4456 Performance of Evolved Acceleration Guidance Logic for Entry (EAGLE)Mease, K. / Saraf, A. / Chen, D. / Leavitt, J. / AIAA et al. | 2002
- 198
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AIAA-2002-4457 Profile-Following Entry Guidance Using Linear Quadratic Regulator TheoryDukeman, G. / AIAA et al. | 2002
- 208
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AIAA-2002-4458 Adaptive Guidance with Trajectory Reshaping for Reusable Launch VehiclesSchierman, J. / Hull, J. / Ward, D. / AIAA et al. | 2002
- 219
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AIAA-2002-4460 A Novel Quaternion Kalman FilterChoukroun, D. / Bar-Itzhack, I. / Oshman, Y. / AIAA et al. | 2002
- 230
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AIAA-2002-4461 State-Dependent Pseudo-Linear Filters for Spacecraft Attitude and Rate EstimationBar-Itzhack, I. / Harman, R. / Choukroun, D. / AIAA et al. | 2002
- 241
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AIAA-2002-4462 Recursive Satellite Attitude Estimation with the Two-Step Optimal EstimatorKasdin, N. / Weaver, T. / AIAA et al. | 2002
- 254
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AIAA-2002-4463 Angular Rate Estimation for Gyroless Satellite Attitude ControlAgrawal, B. / Palermo, W. / AIAA et al. | 2002
- 265
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AIAA-2002-4464 Notes on Observability of Geosynchronous Spacecraft Attitude Determination SystemLi, X. / Goodzeit, N. / AIAA et al. | 2002
- 275
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AIAA-2002-4465 Design and Implementation of a Low Cost, Hierarchical and Modular Avionics Architecture for the DragonFly UAVsJang, J. / Tomlin, C. / AIAA et al. | 2002
- 286
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AIAA-2002-4466 On-Line Estimation and Path Planning for Multiple Vehicles in an Uncertain EnvironmentCampbell, M. / Ousingsawat, J. / AIAA et al. | 2002
- 295
-
AIAA-2002-4468 An Autonomous Hierarchical ControlArchitecture for Unmanned Aerial VehiclesBoskovic, J. / Prasanth, R. / Mehra, R. / AIAA et al. | 2002
- 306
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AIAA-2002-4469 Autonomous Aerial Refueling Utilizing A Vision Based Navigation SystemValasek, J. / Junkins, J. / Kimmett, J. / AIAA et al. | 2002
- 317
-
AIAA-2002-4470 An Algorithmic Implementation of Constrained Extremal Control for UAVsBeard, R. / Anderson, E. / AIAA et al. | 2002
- 327
-
AIAA-2002-4545 A Study on the Design of Reconfigurable Flight Control System Using Input-Output InformationKim, Y. / Kim, H. / Hyung, S. / Kim, S. / AIAA et al. | 2002
- 336
-
AIAA-2002-4546 Linear Parameter Varying Control Synthesis for Actuator Failure, Based on Estimated ParameterShin, J. / Wu, N. / Belcastro, C. / AIAA et al. | 2002
- 347
-
AIAA-2002-4547 High-Fidelity Simulation Testing of Control Allocation MethodsPage, A. / Steinberg, M. / AIAA et al. | 2002
- 357
-
AIAA-2002-4548 Active Failure Management for Aircraft Control RecoveryGlavaski, S. / Elgersma, M. / Dorneich, M. / Lommel, P. / AIAA et al. | 2002
- 367
-
AIAA-2002-4549 A Reconfigurable Nonlinear AutopilotBodson, M. / AIAA et al. | 2002
- 381
-
AIAA-2002-4550 Applied Adaptive Techniques for F/A-18 Formation FlightMisovec, K. / AIAA et al. | 2002
- 391
-
AIAA-2002-4551 Cockpit Multi-Agents for Distributed Air Traffic ManagementPainter, J. / AIAA et al. | 2002
- 402
-
AIAA-2002-4552 An Agent-Based Approach to Aircraft Conflict Resolution with ConstraintsHarper, K. / Guarino, S. / White, A. / Hanson, M. / Bilimoria, K. / Mulfinger, D. / AIAA et al. | 2002
- 413
-
AIAA-2002-4553 Hierarchical Agent Based System for General Aviation CD&R Under Free FlightValasek, J. / Shandy, S. / Rong, J. / Bokadia, S. / AIAA et al. | 2002
- 424
-
AIAA-2002-4554 A Flight Deck Decision Support Tool for Autonomous Airborne OperationsJohnson, E. / Vivona, R. / Sharma, V. / Ramiscal, E. / Ballin, M. / AIAA et al. | 2002
- 435
-
AIAA-2002-4555 Use of Traffic Intent Information by Autonomous Aircraft in Constrained OperationsWing, D. / Barmore, B. / Krishnamurthy, K. / AIAA et al. | 2002
- 449
-
AIAA-2002-4556 Applications of User Intent in Cockpit- and Ground-Based Decision Support ToolsVivona, R. / AIAA et al. | 2002
- 460
-
AIAA-2002-4557 A Plan for Advanced Guidance and Control Technology for 2nd Generation Reusable Launch VehiclesHanson, J. / AIAA et al. | 2002
- 469
-
AIAA-2002-4558 Closed-Loop Endo-Atmospheric Ascent GuidanceLu, P. / Sun, H. / Tsai, B. / AIAA et al. | 2002
- 486
-
AIAA-2002-4559 Atmospheric Ascent Guidance for Rocket-Powered Launch VehiclesDukeman, G. / AIAA et al. | 2002
- 497
-
AIAA-2002-4560 Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization MethodCalise, A. / Brandt, N. / AIAA et al. | 2002
- 508
-
AIAA-2002-4561 Advanced Guidance and Control Methods for Reusable Launch Vehicles: Test ResultsHanson, J. / Jones, R. / AIAA et al. | 2002
- 519
-
AIAA-2002-4562 Autocommander - A Supervisory Controller for Integrated Guidance and Control for the 2nd Generation Reusable Launch VehicleLawrence, D. / Fisher, J. / Zhu, J. / AIAA et al. | 2002
- 530
-
AIAA-2002-4563 Investigation of Target-Speed Adjustment of the Lead Robot in an Adaptively Controlled Multiple Robot FormationJoshi, S. / Riehl, J. / Ganji, F. / AIAA et al. | 2002
- 541
-
AIAA-2002-4564 Feedback Linearization and Predictive Control: A ComparisonTalole, S. / Banavar, R. / AIAA et al. | 2002
- 550
-
AIAA-2002-4565 Methods of Trajectory Tracking for Flexible Link ManipulatorsGreen, A. / Sasiadek, J. / AIAA et al. | 2002
- 561
-
AIAA-2002-4566 A Consideration on Dynamic Constraint of Planar Manipulators with Free-JointsHokamoto, S. / Kawahara, Y. / AIAA et al. | 2002
- 568
-
AIAA-2002-4567 Modeling and Control of a PowerSailVadali, S. / Naik, K. / Alfriend, K. / AIAA et al. | 2002
- 579
-
AIAA-2002-4568 Inertia Parameter Identification for a Free-Flying Space RobotYoshida, K. / Abiko, S. / AIAA et al. | 2002
- 587
-
AIAA-2002-4569 Robust Execution of Aggressive Maneuvers for Planetary RoboticsBretl, T. / Rock, S. / AIAA et al. | 2002
- 595
-
AIAA-2002-4570 Computation and Visualization of Control Moment Gyroscope SingularitiesDominguez, J. / Wie, B. / AIAA et al. | 2002
- 605
-
AIAA-2002-4571 Nonlinear Momentum Transfer Control of Spacecraft by Feedback LinearizationBang, H. / Myung, H. / Tahk, M. / AIAA et al. | 2002
- 616
-
AIAA-2002-4572 Dynamic Modeling and Attitude Control of Solar Sail Spacecraft: Part IWie, B. / AIAA et al. | 2002
- 628
-
AIAA-2002-4573 Dynamic Modeling and Attitude Control of Solar Sail Spacecraft: Part IIWie, B. / AIAA et al. | 2002
- 640
-
AIAA-2002-4574 Directed Momentum Management for Rotating SpacecraftRogers, K. / Ratan, S. / AIAA et al. | 2002
- 648
-
AIAA-2002-4575 Spacecraft Robust Attitude Control with Saturation NonlinearityJuang, J. / Show, L. / Lin, C. / Jan, Y. / AIAA et al. | 2002
- 657
-
AIAA-2002-4576 Robust Spacecraft Attitude Control Using Model-Error Control SynthesisCrassidis, J. / Kim, J. / AIAA et al. | 2002
- 668
-
AIAA-2002-4577 A Constrained Optimization Approach for CMG Robust Flex Filter DesignJang, J. / Bedrossian, N. / Lee, A. / Spanos, P. / AIAA et al. | 2002
- 677
-
AIAA-2002-4578 The Microwave Anisotropy Probe (MAP) MissionMarkley, F. / Andrews, S. / O Donnell, J. / Ward, D. / AIAA et al. | 2002
- 687
-
AIAA-2002-4579 The Microwave Anisotropy Probe Guidance, Navgation and Control Hardware SuiteWard, D. / Davis, G. / O Donnell, J. / AIAA et al. | 2002
- 698
-
AIAA-2002-4580 MAP Attitude Control System Design and Flight PerformanceAndrews, S. / O Donnell, J. / AIAA et al. | 2002
- 707
-
AIAA-2002-4581 An Anomalous Force on the MAP SpacecraftStarin, S. / Bay, P. / Fink, D. / O Donnell, J. / Ward, D. / Wollack, E. / AIAA et al. | 2002
- 718
-
AIAA-2002-4582 Performance of the Microwave Anistropy Probe AST-201 Star TrackersWard, D. / van Bezooijen, R. / AIAA et al. | 2002
- 729
-
AIAA-2002-4583 Restoring Redundancy to the MAP Propulsion SystemO Donnell, J. / Davis, G. / Ward, D. / AIAA et al. | 2002
- 740
-
AIAA-2002-4584 Development of a Two-Wheel Contingency Mode for the MAP SpacecraftStarin, S. / O Donnell, J. / AIAA et al. | 2002
- 750
-
AIAA-2002-4586 Task Allocation for Wide Area Search Munitions via Iterative Network FlowSchumacher, C. / Chandler, P. / Rasmussen, S. / AIAA et al. | 2002
- 758
-
AIAA-2002-4587 Multiple Task Assignment for a UAV TeamChandler, P. / Pachter, M. / Rasmussen, S. / Schumacher, C. / AIAA et al. | 2002
- 768
-
AIAA-2002-4588 Coordination and Control of Multiple UAVsRichards, A. / Bellingham, J. / Tillerson, M. / How, J. / AIAA et al. | 2002
- 779
-
AIAA-2002-4589 A Search-Theoretic Approach to Cooperative Control for Uninhabited Air VehiclesPassino, K. / Baum, M. / AIAA et al. | 2002
- 787
-
AIAA-2002-4590 Decentralized Cooperative Search in UAV's Using Opportunistic LearningMinai, A. / Polycarpou, M. / Yang, Y. / AIAA et al. | 2002
- 797
-
AIAA-2002-4591 A Rule Based Algorithm that Produces Exponentially Stable Formations of Autonomous AgentsMehiel, E. / Balas, M. / AIAA et al. | 2002
- 805
-
AIAA-2002-4646 PID and Fuzzy Logic Pitch Attitude Hold Systems for a Fighter JetBossert, D. / Cohen, K. / AIAA et al. | 2002
- 814
-
AIAA-2002-4647 Attitude Control of a Reentry Vehicle with Internal DynamicsWallner, E. / Well, K. / AIAA et al. | 2002
- 825
-
AIAA-2002-4648 The Conception of Control System Allowing to Modify Small Aircraft's Properties and Simulate Another Plane's BehaviorRogalski, T. / AIAA et al. | 2002
- 833
-
AIAA-2002-4649 Design, Development and Flight Testing of Control Laws for the Indian Light Combat AircraftChetty, S. / Deodhare, G. / Misra, B. / AIAA et al. | 2002
- 844
-
AIAA-2002-4650 MIMO Sliding Mode Control for a Tailless Fighter Aircraft, An Alternative to Reconfigurable ArchitecturesHess, R. / Wells, S. / AIAA et al. | 2002
- 857
-
AIAA-2002-4651 Rapid Prototyping Tools for Commercial AutopilotsRao, S. / Chetty, S. / AIAA et al. | 2002
- 864
-
AIAA-2002-4653 Development and Flight Testing of GNC Algorithms Using a Rapid Flight Test Prototyping SystemYakimenko, O. / Kaminer, I. / Dobrokhodov, V. / Lim, B. / AIAA et al. | 2002
- 874
-
AIAA-2002-4654 Hybrid Guidance Laws for Improved Missile Intercept RangesHutchins, R. / Broadston, R. / Titus, H. / Swee, J. / AIAA et al. | 2002
- 884
-
AIAA-2002-4655 Coordinated Attitude and Formation Control of Multi-Satellite SystemsKang, W. / Sparks, A. / AIAA et al. | 2002
- 891
-
AIAA-2002-4656 Method of Slewing the Spacecraft to Minimize Settling TimeAgrawal, B. / Chen, H. / AIAA et al. | 2002
- 902
-
AIAA-2002-4657 Real-Time Computation of Neighboring Optimal Control LawsRoss, I. / Yan, H. / Fahroo, F. / AIAA et al. | 2002
- 909
-
AIAA-2002-4658 Improving Transient Performance of Dynamic Inversion Missile Autopilot by Use of BacksteppingMichalka, G. / Steinicke, A. / AIAA et al. | 2002
- 918
-
AIAA-2002-4659 Fuzzy Gain-Scheduling Flight Controller for a STT MissileTsourdos, A. / White, B. / AIAA et al. | 2002
- 925
-
AIAA-2002-4661 Integrated Autopilot Tuning Methodology for Airframe Parametric SimulationsLestage, R. / Lauzon, M. / Jeffrey, A. / AIAA et al. | 2002
- 936
-
AIAA-2002-4662 RLV Aero Surfaces Optimization Subject to Stability and Control ConstraintsYoussef, H. / Chowdhry, R. / Lee, H. / Carty, A. / AIAA et al. | 2002
- 944
-
AIAA-2002-4663 Optimal Control of Nonlinear Dynamical Systems Using Direct Solution of Neural Network ControllersPourtakdoust, S. / Zahedi, A. / Jalali, M. / Ghorbani, R. / AIAA et al. | 2002
- 951
-
AIAA-2002-4664 A Neural Network Based Design of Optimal Controllers for Nonlinear SystemsPhan, M. / Kulkarni, N. / AIAA et al. | 2002
- 962
-
AIAA-2002-4665 Discrete-Time Optimal Control Systems with State ConstraintsMurillo, M. / Naidu, S. / AIAA et al. | 2002
- 971
-
AIAA-2002-4666 Design of Autoland Controller Functions with Multi-Objective OptimizationLooye, G. / Joos, H. / AIAA et al. | 2002
- 982
-
AIAA-2002-4667 Improving Control Allocation Accuracy for Nonlinear Aircraft DynamicsDoman, D. / Oppenheimer, M. / AIAA et al. | 2002
- 992
-
AIAA-2002-4668 Data-Based Cost-To-Go Design for Optimal ControlPhan, M. / Kulkarni, N. / AIAA et al. | 2002
- 1002
-
AIAA-2002-4669 Performance Based Evaluation of Star Catalog Generation MethodsPrakash, A. / Wu, A. / Liu, J. / Li, R. / AIAA et al. | 2002
- 1007
-
AIAA-2002-4670 Ground-Based SIAD Software Tool Development for GOES Post-Launch Test SupportLam, Q. / Woodruff, C. / Ashton, S. / Martin, D. / AIAA et al. | 2002
- 1018
-
AIAA-2002-4671 Failure Detection and Isolation Algorithms for the ATV Gyro AssemblyDussy, S. / Fau, N. / Chabert, F. / Gmerek, P. / Strandmoe, S. / AIAA et al. | 2002
- 1027
-
AIAA-2002-4672 Dynamics of Vibratory MicrogyroscopesPloen, S. / Bayard, D. / AIAA et al. | 2002
- 1037
-
AIAA-2002-4673 Autoreturn Function for a Remotely Piloted VehicleMcMinn, J. / Jackson, E. / AIAA et al. | 2002
- 1048
-
AIAA-2002-4674 Trajectory Reconfiguration for an Unmanned AircraftValenti, M. / Mettler, B. / Schouwenaars, T. / Feron, E. / Paduano, J. / AIAA et al. | 2002
- 1055
-
AIAA-2002-4675 Investigation of Single vs. Multiple Task Tour Assignments for UAV Cooperative ControlRasmussen, S. / Chandler, P. / Schumacher, C. / AIAA et al. | 2002
- 1062
-
AIAA-2002-4676 Agile Control of Military Operations (JFACC)Wohletz, J. / Castanon, D. / Curry, M. / AIAA et al. | 2002
- 1073
-
AIAA-2002-4678 Experimental Demonstration of Multiple Robot Cooperative Target InterceptMcLain, T. / Beard, R. / Kelsey, J. / AIAA et al. | 2002
- 1080
-
AIAA-2002-4747 Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft - Part I: System ModelingMeirovitch, L. / Tuzcu, I. / AIAA et al. | 2002
- 1098
-
AIAA-2002-4748 Fuzzy Gain-Scheduled H-infinity Flight Control Law DesignOosterom, M. / Bergsten, P. / Babuska, R. / AIAA et al. | 2002
- 1109
-
AIAA-2002-4749 Controllability Region Analysis for Unstable Aircraft DynamicsGoman, M. / Demenkov, M. / AIAA et al. | 2002
- 1120
-
AIAA-2002-4750 Optimal Blending Filter Parameters and Sensor Placement for Flight ControlNewman, B. / Al-Shehabi, A. / AIAA et al. | 2002
- 1129
-
AIAA-2002-4751 Aircraft Flight Dynamics Analysis and Controller Design Using Bifurcation TailoringLowenberg, M. / Charles, G. / Stoten, D. / Wang, X. / di Bernardo, M. / AIAA et al. | 2002
- 1140
-
AIAA-2002-4752 A Roll Autopilot for Autonomous Air RefuelingAwni, K. / Johnson, K. / AIAA et al. | 2002
- 1148
-
AIAA-2002-4753 On Control of Autonomous Circular ParachutesYakimenko, O. / Dobrokhodov, V. / Johnson, J. / Benney, R. / Dellicker, S. / Kaminer, I. / AIAA et al. | 2002
- 1164
-
AIAA-2002-4754 Fundamental Principles of Alerting Algorithm Design with Applications in Rotorcraft Formation FlightZhao, Y. / Rock, D. / AIAA et al. | 2002
- 1175
-
AIAA-2002-4755 An Overview of Flight Test Results for a Formation Flight AutopilotHanson, C. / Ryan, J. / Allen, M. / Jacobson, S. / AIAA et al. | 2002
- 1189
-
AIAA-2002-4756 String Stability of a Linear Formation Flight Control SystemAllen, M. / Ryan, J. / Parle, J. / Hanson, C. / AIAA et al. | 2002
- 1201
-
AIAA-2002-4757 F/A-18 Autonomous Formation Flight Control System DesignLavretsky, E. / AIAA et al. | 2002
- 1209
-
AIAA-2002-4758 Implementation of Control Algorithms in an Environment of Dynamically Scheduled CPU Time Using Balanced TruncationBhattacharya, R. / Balas, G. / AIAA et al. | 2002
- 1214
-
AIAA-2002-4759 LPV Controller Interpolation for Improved Gain-Scheduling Control PerformanceWu, F. / Kim, S. / AIAA et al. | 2002
- 1224
-
AIAA-2002-4760 Decoupling of Nonminimum Phase Plants and Application to Flight ControlSnell, A. / AIAA et al. | 2002
- 1231
-
AIAA-2002-4761 Dynamic Control Allocation Using Constrained Quadratic ProgrammingHarkegard, O. / AIAA et al. | 2002
- 1241
-
AIAA-2002-4762 Tuning of A Random Search Algorithm for Controller DesignKumar, R. / Hyland, D. / AIAA et al. | 2002
- 1249
-
AIAA-2002-4763 LTV Approach to Satellite Attitude Control Using Only Magnetic ActuationJafarboland, M. / Sadati, N. / Momeni, H. / AIAA et al. | 2002
- 1257
-
AIAA-2002-4764 A Method for Genterating Multi-Center TrajectoriesMurphy, J. / Reisman, R. / Clayton, J. / AIAA et al. | 2002
- 1266
-
AIAA-2002-4765 Strategic Aircraft Trajectory Prediction Uncertainty and Statistical Sector Traffic Load ModelingMuller, T. / Sorensen, J. / Couluris, G. / AIAA et al. | 2002
- 1277
-
AIAA-2002-4766 Probabilistic Methods for Air Traffic Demand ForecastingMeyn, L. / AIAA et al. | 2002
- 1292
-
AIAA-2002-4767 A Study on the Feasibility of Using a Genetic Algorithm to Generate Realistic Air Traffic Scenarios Based on Recorded Field DataOaks, R. / AIAA et al. | 2002
- 1300
-
AIAA-2002-4768 Delay Distribution in a Multi-Center/Multi-Sector EnvironmentSlater, G. / AIAA et al. | 2002
- 1310
-
AIAA-2002-4769 Short Term Effects of a Volcanic Eruption in Iceland on Air Traffic and Air Traffic ControlSveinbjornsson, M. / Palsson, A. / Arnarson, B. / Hauksdottir, A. / AIAA et al. | 2002
- 1321
-
AIAA-2002-4770 Improving the High Altitude Performance of Tail-Controlled Endoatmospheric MissilesZarchan, P. / Greenberg, E. / Alpert, J. / AIAA et al. | 2002
- 1332
-
AIAA-2002-4772 Nonlinear Target State Estimation in Homing GuidanceTalole, S. / Phadke, S. / AIAA et al. | 2002
- 1341
-
AIAA-2002-4773 Nonlinear Guidance and Navigation of a Tactical Missile with High Heading ErrorTaur, D. / AIAA et al. | 2002
- 1360
-
AIAA-2002-4774 Performance Analysis of Nominal Scheme and Decoupling Loop Scheme for RF SeekerBhattacharyya, A. / Bhattacharjee, R. / AIAA et al. | 2002
- 1371
-
AIAA-2002-4775 Footprint Determination for Reusable Launch Vehicles Experiencing Control Effector Failures (Invited)Ngo, A. / Doman, D. / AIAA et al. | 2002
- 1379
-
AIAA-2002-4776 A Six Degree-of-Freedom Adaptive Flight Control Architecture for Trajectory FollowingJohnson, E. / Corban, J. / Calise, A. / AIAA et al. | 2002
- 1390
-
AIAA-2002-4777 Autonomous Reconfigurable Control Allocation (ARCA) for Reusable Launch VehiclesHodel, A. / Callahan, R. / AIAA et al. | 2002
- 1398
-
AIAA-2002-4778 Direct Fault Tolerant RLV Attitude Control - A Singular Perturbation ApproachZhu, J. / Lawrence, D. / Fisher, J. / Lu, P. / Shtessel, Y. / Hodel, A. / AIAA et al. | 2002
- 1409
-
AIAA-2002-4779 Reusable Launch Vehicle Attitude Control Using Time-Varying Sliding ModesShtessel, Y. / Zhu, J. / Daniels, D. / AIAA et al. | 2002
- 1419
-
AIAA-2002-4780 On-Line Computation of a Local Attainable Moment Set for Reusable Launch VehiclesHodel, A. / Shtessel, Y. / AIAA et al. | 2002
- 1426
-
AIAA-2002-4781 L2-Gain and Stability Analysis for a Rigid Spacecraft Under Gravity-Gradient TorqueDamaren, C. / AIAA et al. | 2002
- 1431
-
AIAA-2002-4782 Solar Precession Dynamics of a Spinning SpacecraftLim, T. / DeLaHunt, P. / AIAA et al. | 2002
- 1442
-
AIAA-2002-4783 Advanced Harmonic Analysis of Nonlinear Spacecraft Control SystemsLim, S. / Chan, K. / AIAA et al. | 2002
- 1452
-
AIAA-2002-4784 New Methodology for Single Parameter Robust Spacecraft Control Analysis and SynthesisNewman, B. / Player, C. / AIAA et al. | 2002
- 1463
-
AIAA-2002-4785 Attitude Dynamics and Control of Space Cargo for Reusable Orbital Logistic Supply ServicingMatsumoto, S. / Oda, M. / Kawano, I. / AIAA et al. | 2002
- 1470
-
AIAA-2002-4834 Control Logic for Automated Aerobatic Flight of a Miniature HelicopterGavrilets, V. / Mettler, B. / Feron, E. / Martinos, I. / AIAA et al. | 2002
- 1478
-
AIAA-2002-4836 Design and Flight Testing of a High-Bandwidth H-Infinity Loop Shaping Controller for a Robotic HelicopterLa Civita, M. / Papageorgiou, G. / Messner, W. / Kanade, T. / AIAA et al. | 2002
- 1489
-
AIAA-2002-4837 Reconfigurable Helicopter Flight Control Methods for Main Rotor Actuator FailuresSi, J. / Enns, R. / AIAA et al. | 2002
- 1504
-
AIAA-2002-4839 Trajectory Shaping and Terminal Guidance Using Linear Quadratic Differential GamesBen-Asher, J. / Levinson, S. / Weiss, H. / AIAA et al. | 2002
- 1514
-
AIAA-2002-4840 A Near Optimal Midcourse Guidance Law Based on Spherical GravityDeihoul, A. / Massoumnia, M. / AIAA et al. | 2002
- 1521
-
AIAA-2002-4841 Linear Quadratic Guidance Laws for Missiles Having Dual Control SystemsShima, T. / Golan, O. / AIAA et al. | 2002
- 1532
-
AIAA-2002-4842 An Approximate Target Adaptive Guidance for IR HomingKim, P. / Jun, B. / Cho, H. / AIAA et al. | 2002
- 1539
-
AIAA-2002-4844 Optimal Two-Impulse Rendezvous Between Two Circular Orbits Using Multiple-Revolution Lambert's SolutionsTsiotras, P. / Shen, H. / AIAA et al. | 2002
- 1550
-
AIAA-2002-4845 Influence of the ATV Propellant Sloshing on the GNC PerformanceBayle, O. / L Hullier, V. / Ganet, M. / Delpy, P. / Francart, J. / Paris, D. / AIAA et al. | 2002
- 1560
-
AIAA-2002-4846 Autonomous Acquisition, Rendezvous, & Docking Using a Video Guidance Sensor: Experimental Testbed ResultsKeller, B. / Tadikonda, S. / Mapar, J. / AIAA et al. | 2002
- 1570
-
AIAA-2002-4847 An Analytical Approach to Analyzing Spacecraft Formation-Flying MotionZhang, H. / Xu, B. / Zhang, Z. / AIAA et al. | 2002
- 1576
-
AIAA-2002-4848 Effects of Controls Degradation on Flight Mission of Reentry VehicleCosta, O. / Sachs, G. / AIAA et al. | 2002
- 1584
-
AIAA-2002-4849 Control Allocation for the Next Generation of Entry VehiclesShertzer, R. / Zimpfer, D. / Brown, P. / AIAA et al. | 2002
- 1594
-
AIAA-2002-4850 Robust Guaranteed Cost Control for Discrete-Time Systems with Multiple Delays in StateAgarwal, R. / Shi, Y. / Lin, Z. / Shi, P. / AIAA et al. | 2002
- 1607
-
AIAA-2002-4851 Robust Kalman Filtering for Jump Continuous Time-Lag SystemsAgarwal, R. / Shi, P. / Mahmoud, M. / AIAA et al. | 2002
- 1620
-
AIAA-2002-4852 A Design Method for a Robust LQ Optimal Model-Following ControllerSato, M. / AIAA et al. | 2002
- 1630
-
AIAA-2002-4853 Gain-Scheduling H-infinity Control of the Launcher in Atmospheric Flight via Linear-Parameter Varying TechniquesVoinot, O. / Apkarian, P. / Alazard, D. / AIAA et al. | 2002
- 1641
-
AIAA-2002-4854 Design of Robust Autoland Control Laws Using Mu-SynthesisLooye, G. / Sancho, C. / Makdoembaks, A. / Mulder, J. / AIAA et al. | 2002
- 1652
-
AIAA-2002-4856 Automation Tools for Enhancing Ground-Operation Situation Awareness and Flow EfficiencyCheng, V. / Foyle, D. / AIAA et al. | 2002
- 1663
-
AIAA-2002-4857 Improved Taxi Prediction Algorithms for the Surface Management SystemBrinton, C. / Krozel, J. / Capozzi, B. / Atkins, S. / AIAA et al. | 2002
- 1674
-
AIAA-2002-4858 Advanced Noise Abatement Procedures for Approach and DepartureErkelens, L. / AIAA et al. | 2002
- 1683
-
AIAA-2002-4859 Flight Trials: "Runway-to-Runway" Required Time of Arrival Evaluations for Time-Based ATM Environment - Final ResultsWichman, K. / Carlsson, G. / Lindberg, L. / AIAA et al. | 2002
- 1694
-
AIAA-2002-4860 Limited Delegation with Arrival Streams: More Insight on its Impact on Controller ActivityHoffman, E. / Grimaud, I. / Rognin, L. / Zeghal, K. / AIAA et al. | 2002
- 1704
-
AIAA-2002-4861 Design and Preliminary Evaluation of a Segment-Based Routing MethodologyVormer, F. / Mulder, M. / van Paassen, R. / Mulder, J. / AIAA et al. | 2002
- 1715
-
AIAA-2002-4917 Adaptive Compensation for Flexible DynamicsCalise, A. / Kim, N. / Buffington, J. / AIAA et al. | 2002
- 1723
-
AIAA-2002-4918 An Adaptive Output Feedback Control Methodology: Theory and Practical Implementation AspectsIdan, M. / Calise, A. / Hovakimyan, N. / AIAA et al. | 2002
- 1734
-
AIAA-2002-4919 Adaptive Actuator Failure Compensation for Parametric Strict Feedback Systems and an Aircraft ApplicationTao, G. / Tang, X. / AIAA et al. | 2002
- 1744
-
AIAA-2002-4920 A Discrete Time Adaptive Disturbance Rejection and Control Algorithm Applied to a Model of a Deployable Space TelescopeMehiel, E. / Balas, M. / Fuentes, R. / AIAA et al. | 2002
- 1753
-
AIAA-2002-4921 Experimental Results on Adaptive Output Feedback Control Using a Laboratory Model HelicopterCalise, A. / Kutay, A. / Idan, M. / Hovakimyan, N. / AIAA et al. | 2002
- 1760
-
AIAA-2002-4922 Evolutionary Optimisation of a Model Reference Adaptive Control SystemMooij, E. / AIAA et al. | 2002
- 1771
-
AIAA-2002-4924 Low-Cost 3D-Display and Navigation System for Small AircraftSachs, G. / Sperl, R. / AIAA et al. | 2002
- 1779
-
AIAA-2002-4925 Pursuit Display Review and Extension to a Civil Tilt Rotor Flight DirectorHardy, G. / AIAA et al. | 2002
- 1789
-
AIAA-2002-4926 Flight Management VNAV-Approach PathsKaratsinides, S. / AIAA et al. | 2002
- 1794
-
AIAA-2002-4927 Dynamics of Self-Spacing in a Stream of In-Trail AircraftSlater, G. / AIAA et al. | 2002
- 1803
-
AIAA-2002-4928 Fly-by-wire Control and Tunnel-in-the-Sky Displays: Towards a Task-Oriented Control/Display SystemMulder, M. / Veldhuijzen, A. / van Paassen, R. / Bennani, S. / AIAA et al. | 2002
- 1814
-
AIAA-2002-4929 Delft Aerospace Tunnel-in-the-Sky Flight TestsMulder, M. / Kraeger, A. / Soijer, M. / AIAA et al. | 2002
- 1824
-
AIAA-2002-4930 Corridor Integrated Weather System (CIWS) Cockpit Weather Display Data Link DemonstrationCampbell, S. / Grappel, R. / Hoffman, M. / Hogaboom, R. / Lloyd, R. / O Rourke, J. / AIAA et al. | 2002
- 1835
-
AIAA-2002-4931 Open System Protocols for Aviation Data Link ApplicationsGrappel, R. / AIAA et al. | 2002
- 1845
-
AIAA-2002-4932 Newly Enacted Intent Changes to ADS-B MASPS: Emphasis on Operations, Compatibility, and IntegrityBarhydt, R. / Warren, A. / AIAA et al. | 2002
- 1853
-
AIAA-2002-4933 Impact of ADS-B Link Characteristics on the Performances of In-Trail Following AircraftHoffman, E. / Ivanescu, D. / Zeghal, K. / AIAA et al. | 2002
- 1862
-
AIAA-2002-4934 Multisource Flight Surveillance Radar Data FusionHauksdottir, A. / Guogeirsson, J. / Simonarson, P. / AIAA et al. | 2002
- 1869
-
AIAA-2002-4935 Estimation of Radar Errors and Correction of Flight TracksHauksdottir, A. / Arnarson, B. / Botzelmann, S. / AIAA et al. | 2002
- 1875
-
AIAA-2002-4936 Docked Two-Vehicle Dynamics, and Control by One-Vehicle: Experimental ResultsTadikonda, S. / Keller, B. / Mapar, J. / AIAA et al. | 2002
- 1886
-
AIAA-2002-4937 System Identification of a Nonlinear Flexible Mode for the Shuttle Radar Topography MissionBayard, D. / Brugarolas, P. / Spanos, J. / Breckenridge, W. / AIAA et al. | 2002
- 1897
-
AIAA-2002-4938 Robust Flutter Analysis of an F-16A/B in Heavy Store ConfigurationBeuker, B. / Bennani, S. / van Staveren, J. / Meijer, J. / AIAA et al. | 2002
- 1912
-
AIAA-2002-4939 Local and Hierarchic Control for Active and Adaptive OpticsMacMartin, D. / AIAA et al. | 2002
- 1923
-
AIAA-2002-4940 A Convex Approach to Fault Tolerant ControlMaghami, P. / Cox, D. / AIAA et al. | 2002
- 1932
-
AIAA-2002-4941 Concurrent Feed-forward/Feed-back Design for Flexible StructuresSingh, T. / Muenchhof, M. / AIAA et al. | 2002
- 1940
-
AIAA-2002-4942 An Augmenting Adaptive Approach to Control of Flexible SystemsCalise, A. / Yang, B. / Craig, J. / AIAA et al. | 2002
- 1950
-
AIAA-2002-4943 Minimax Design of Prefilters for Maneuvering Flexible StructuresSingh, T. / Kuo, Y. / AIAA et al. | 2002
- 1958
-
AIAA-2002-4944 Application of H-infinity Fault Detection and Isolation to a Boeing 747-100/200 AircraftMarcos, A. / Ganguli, S. / Balas, G. / AIAA et al. | 2002
- 1967
-
AIAA-2002-4945 Towards Real-Time Computation of Optimal Controls for Nonlinear SystemsStrizzi, J. / Ross, I. / Fahroo, F. / AIAA et al. | 2002
- 1977
-
AIAA-2002-4946 Correlation and Convergence of Inertial Navigation System Error ModelsRogers, R. / AIAA et al. | 2002
- 1988
-
AIAA-2002-4947 Optimal Missile Avoidance Trajectory Synthesis in the EndgameRanta, J. / Raivio, T. / AIAA et al. | 2002
- 1999
-
AIAA-2002-4949 A New Differential-Game Based Guidance Law Using Target Orientation ObservationsOshman, Y. / Arad, D. / AIAA et al. | 2002
- 2009
-
AIAA-2002-4950 Boost Phase Identification of Theatre Ballistic Missiles Using RADAR MeasurementsOshman, Y. / Almogi-Nadler, M. / Ben-Asher, J. / AIAA et al. | 2002
- 2019
-
AIAA-2002-4951 Modified Guidance with N-Fixed-Interval Propulsive ManeuversJalali-Naini, S. / Ebrahimi, B. / AIAA et al. | 2002
- 2026
-
AIAA-2002-4952 Optimal Mean Squared Error ImagingKabamba, P. / Hyland, D. / Chakravorty, S. / AIAA et al. | 2002
- 2035
-
AIAA-2002-4955 Fault Detection and Isolation for Spacecraft - Geometric ApproachJensen, H. / Wisniewski, R. / AIAA et al. | 2002
- 2043
-
AIAA-2002-4956 Verification of Real Time Collision Avoidance for HelicoptersLin, C. / Hung, S. / AIAA et al. | 2002
- 2051
-
AIAA-2002-4957 LPV Detection Filter Design for Boeing 747-100/200Szaszi, I. / Marcos, A. / Balas, G. / Bokor, J. / AIAA et al. | 2002
- 2057
-
AIAA-2002-4958 Planning Algorithm for Large Satellite ClustersCampbell, M. / AIAA et al. | 2002
- 2066
-
AIAA-2002-4959 Partially Decentralized Control Architectures for Satellite FormationsCarpenter, J. / AIAA et al. | 2002
- 2077
-
AIAA-2002-4960 An Optimal Guidance Law for Formation Flying and StationkeepingD Souza, C. / AIAA et al. | 2002
- 2083
-
AIAA-2002-4961 New Formation Flying Testbed for Analyzing Distributed Estimation and Control ArchitecturesFerguson, P. / Yang, T. / Tillerson, M. / How, J. / AIAA et al. | 2002
- 2094
-
AIAA-2002-4962 Neurocontrol of Spacecraft Formation Flying in the Elliptic Restricted Three-Body ProblemGurfil, P. / Idan, M. / Kasdin, N. / AIAA et al. | 2002
- 2105
-
AIAA-2002-4963 Virtual Structure Based Spacecraft Formation Control with Formation FeedbackBeard, R. / Ren, W. / AIAA et al. | 2002
- 2113
-
AIAA-2002-4964 GN&C Systems for GUARDIAN: Micro-Satellite in a LEO Swarm/FormationStrizzi, J. / Chernesky, V. / Damphousse, P. / Bermingham, D. / Travis, H. / Kutrieb, J. / AIAA et al. | 2002
- 2124
-
AIAA-2002-4993 Waypoint-Based Fuzzy Guidance for Unmanned Aircraft a New ApproachPollini, L. / Baralli, F. / Innocenti, M. / AIAA et al. | 2002
- 2132
-
AIAA-2002-4995 Intelligent Tracking of Aircraft in the National Airspace SystemKrozel, J. / AIAA et al. | 2002
- 2141
-
AIAA-2002-4996 On-Line Learning RBF Neural Networks for Sensor ValidationCampa, G. / Napolitano, M. / Wan, S. / Fravolini, M. / AIAA et al. | 2002
- 2148
-
AIAA-2002-4997 The Rough Sets Theory in Diagnostic Aircraft Control and Navigation SystemsDolega, B. / AIAA et al. | 2002
- 2152
-
AIAA-2002-4998 The Aerospace Corporation Beam Steering Testing FacilityDunbar, C. / AIAA et al. | 2002
- 2160
-
AIAA-2002-4999 Alternate Beam Control Using Bragg Cell DiffractionSullins, A. / Rogers, R. / Ly, J. / Dunbar, C. / AIAA et al. | 2002
- 2168
-
AIAA-2002-5000 Performance Evaluation of a Precision Pointing PayloadOr, A. / Wong, R. / Atmadja, R. / Ly, J. / AIAA et al. | 2002
- 2173
-
AIAA-2002-5001 Robust Multiloop Gain and Phase Margin Calculation Using mu Analysis and Spacecraft ApplicationLy, J. / AIAA et al. | 2002
- 2177
-
AIAA-2002-5002 Inertial Beam Alignment Sensor and a Simplified ApplicationDahl, P. / AIAA et al. | 2002
- 2185
-
AIAA-2002-5003 Real-Time Experimental Demonstration of Precise Decentralized Relative Navigation for Formation Flying SpacecraftBusse, F. / How, J. / AIAA et al. | 2002
- 2196
-
AIAA-2002-5004 GPS-Based Navigation and Orbit Determination for AMSAT AO-40 SatelliteDavis, G. / Moreau, M. / Carpenter, R. / Bauer, F. / AIAA et al. | 2002
- 2207
-
AIAA-2002-5005 Tightly-Coupled IMU/GPS Re-Entry Navigation SystemMooij, E. / Chu, Q. / AIAA et al. | 2002
- 2218
-
AIAA-2002-5008 Development of Guidance Systems in IsraelBar-Itzhack, I. / AIAA et al. | 2002
- 2225
-
AIAA-2002-5010 Background, Description and Significance of the Launch of the Explorer I, United States First Satelite SystemBates, D. / AIAA et al. | 2002
- 2232
-
AIAA-2002-5011 A Control Theoretic Predictive Model for Sector-Based Air Traffic FlowTomlin, C. / Grieder, P. / Bayen, A. / AIAA et al. | 2002
- 2243
-
AIAA-2002-5012 A New Approach for Modeling, Analysis and Control of Air Traffic FlowMenon, P. / Sweriduk, G. / Bilimoria, K. / AIAA et al. | 2002
- 2254
-
AIAA-2002-5013 Conflict-Free Conformance to En Route Flow Rate ConstraintsFeron, E. / Dugail, D. / Bilimoria, K. / AIAA et al. | 2002
- 2265
-
AIAA-2002-5014 Integration of Traffic Flow Management DecisionsChatterji, G. / Sheth, K. / Sridhar, B. / Grabbe, S. / AIAA et al. | 2002
- 2274
-
AIAA-2002-5015 Decision Support for Complex Traffic Flow Management Actions: Integrated Impact AssessmentWanke, C. / Miller, S. / Rhodes, L. / DeArmon, J. / Taber, N. / Berry, D. / Yee, M. / AIAA et al. | 2002
- 2284
-
AIAA-2002-5016 Analysis of En Route Sector Demand Error SourcesKrozel, J. / Rosman, D. / Grabbe, S. / AIAA et al. | 2002
- 2295
-
AIAA-2002-5019 Design and Analysis of the g-LIMIT Baseline Vibration Isolation Control SystemWhorton, M. / Kim, Y. / Jackson, M. / AIAA et al. | 2002
- 2302
-
AIAA-2002-5020 Optimal Control Design Using an H2 Method for the Glovebox Integrated Microgravity Isolation Technology (g-LIMIT)Calhoun, P. / Hampton, D. / AIAA et al. | 2002
- 2311
-
AIAA-2002-5022 Optimal Passive and Active Target Tracking Using the Two-Step EstimatorGurfil, P. / Kasdin, N. / AIAA et al. | 2002
- 2319
-
AIAA-2002-5023 A New Optimal Nonlinear Control Method and its Application to Missile Guidance Law DesignBalakrishnan, S. / Xin, M. / AIAA et al. | 2002
- 2329
-
AIAA-2002-5024 3D Nonlinear H2/H-inf Guidance Law with Dissipative TheoryChen, H. / Yang, C. / AIAA et al. | 2002
- 2336
-
AIAA-2002-5025 Guidance, Navigation and Control Without Gyros: A Gun-Launched Munition ConceptOhlmeyer, E. / Fraysse, J. / Pepitone, T. / AIAA et al. | 2002
- 2350
-
AIAA-2002-5026 Vision-Augmented GNC: Passive Ranging from Image FlowMarkel, M. / Evers, J. / Lopez, J. / Gebert, G. / AIAA et al. | 2002
- 2358
-
AIAA-2002-5027 Disturbance-Free Payload Concept DemonstrationPedreiro, N. / Clappier, R. / Gonzales, M. / Carrier, A. / Lorell, K. / Roth, D. / Shelef, G. / AIAA et al. | 2002
- 2370
-
AIAA-2002-5028 On the Control Design of the Disturbance Reduction System for the Lisa MissionPiper, G. / Watkins, J. / Leitner, J. / Markley, F. / AIAA et al. | 2002
- 2381
-
AIAA-2002-5029 Spacecraft Architecture for Disturbance-Free PayloadPedreiro, N. / AIAA et al. | 2002
- 2393
-
AIAA-2002-5030 Tracking and Pointing of Target by a Bifocal Relay Mirror Spacecraft Using Attitude Control and Fast Steering Mirrors TiltingRomano, M. / Agrawal, B. / AIAA et al. | 2002
- 2405
-
AIAA-2002-5031 Bifocal Relay Mirror Experiments on the NPS Three Axis Spacecraft SimulatorSpencer, M. / Chernesky, V. / Baker, J. / Romano, M. / AIAA et al. | 2002
- 2414
-
AIAA-2002-5032 Optical Alignment of Autonomous Model Spacecraft Triad Using Rule-Based Controls: Experimental StudyWang, P. / Yee, J. / Sayegh, E. / Hadaegh, F. / AIAA et al. | 2002
- 2425
-
AIAA-2002-5047 Recent Flight Results of the TRMM Kalman FilterAndrews, S. / Bilanow, S. / AIAA et al. | 2002
- 2436
-
AIAA-2002-5053 Atom Inferometer-Based Inertial Force SensorsKasevich, M. / Fixler, J. / Bongs, K. / Young, B. / Foster, G. / AIAA et al. | 2002
- 2442
-
AIAA-2002-5054 Three Axis Authority Momentum Spacecraft Attitude ControlBarker, L. / Rodden, J. / Price, X. / AIAA et al. | 2002
- 2451
-
AIAA-2002-5055 Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft - Part II: Control DesignMeirovitch, L. / Tuzcu, I. / AIAA et al. | 2002
- 2468
-
AIAA-2002-5057 Reduction of Earth Sensor Random Error Caused by Minute Vibration InterferenceNigo, K. / Hasegawa, R. / Kurii, T. / Fukui, M. / AIAA et al. | 2002