Extensions to the Galileo Attitude Control System for the Probe Mission (Englisch)
- Neue Suche nach: Neilson, T.
- Neue Suche nach: Hilbert, K.
- Neue Suche nach: Neilson, T.
- Neue Suche nach: Hilbert, K.
- Neue Suche nach: Culp, R. D.
- Neue Suche nach: Odefey, M. L.
In:
Advances in the astronautical sciences
;
647-666
;
1996
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ISBN:
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ISSN:
- Aufsatz (Konferenz) / Print
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Titel:Extensions to the Galileo Attitude Control System for the Probe Mission
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Beteiligte:
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Kongress:Annual Rocky Mountain guidance and control conferences; 19th, Advances in the astronautical sciences ; 1996 ; Breckenridge; CO
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Erschienen in:Advances in the astronautical sciences ; 647-666ADVANCES IN THE ASTRONAUTICAL SCIENCES ; 92 ; 647-666
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Verlag:
- Neue Suche nach: Univelt, Incorporated
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Erscheinungsdatum:01.01.1996
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Format / Umfang:20 pages
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ISBN:
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ISSN:
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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.
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- 39
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Autonomous Navigation Integrated With Spacecraft Communication SystemsGramling, C. J. / Long, A. C. / Horstkamp, G. M. et al. | 1996
- 57
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Implementing Autonomous Orbit ControlWertz, J. R. et al. | 1996
- 69
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Autonomous Spacecraft Orbit Determination Using the Magnetic Field and Attitude InformationKetchum, E. et al. | 1996
- 83
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Hemispherical Resonator Gyro Noise Reduction for Precision Spacecraft PointingMatthews, A. / Bauer, D. A. et al. | 1996
- 101
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Analysis of the CT-633 Star Tracker's Attitude Estimation CapabilityBank, T. / Gravseth, I. J. et al. | 1996
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The Hemispherical Resonator Gyro-A User's PerspectiveGoodzeit, N. E. / Throckmorton, A. J. / Pijaca, J. / Wright, D. et al. | 1996
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Flight System Testbed Verification of the Mars Pathfinder Attitude Control SystemBasilio, R. R. et al. | 1996
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The Attitude Control System Test-Bed for SWAS and Future SMEX MissionsZimbelman, D. / Anderson, M. / Correll, T. / Schnurr, R. et al. | 1996
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System Identification Methods for the Developmental of Experimentally-Based Control Systems on the Space Integrated Controls Experiment (SPICE) TestbedNinneman, R. R. / Baldwin, R. D. / Blankinship, R. M. et al. | 1996
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The Mars Global Surveyor Spacecraft Test LaboratoryPatel, K. et al. | 1996
- 189
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GPS Based Attitude Determination for Spacecraft: System Engineering Design Study and Ground Testbed Results, George E. SevastonCraymer, L. / Breckenridge, W. et al. | 1996
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Experimental Investigation of Robust Control of Flexible Space StructuresWhorton, M. / Calise, A. J. et al. | 1996
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The use of Hardware Emulation Systems for Control Systems Research and EducationVagners, J. et al. | 1996
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Mission Performance, Guidance, and Control of a Genetic Airbreathing Launch VehicleSchmidt, D. K. et al. | 1996
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An Autonomous System for Mitigating Earth Radiance ErrorsDiedrickson, N. / Rullman, G. / Anderson, L. et al. | 1996
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New Technologies for Satellite Inertial Reference SystemsTaylor, W. L. et al. | 1996
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Active System for Vibration Isolation of Spacecraft InstrumentsAnderson, E. H. / Leo, D. J. / Holcomb, M. D. et al. | 1996
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Design and Testing of a Broadband Active Vibration Isolation System Using Stiff ActuatorsHenderson, T. C. et al. | 1996
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Micro-Precision Interferometer Testbed: Fringe Tracker Control SystemNeat, G. W. / O'Brien, J. F. et al. | 1996
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Shape Memory Actuated Spacecraft MechanismsCarpenter, B. F. / Clark, C. R. / Draper, J. L. et al. | 1996
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Applications of Robust Damping Treatments to Advanced Spacecraft StructuresNye, T. W. / Bronowicki, A. J. / Manning, R. A. / Simonian, S. S. et al. | 1996
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A Multiple-Input, Multiple-Output Neural Architecture for the Suppression of a Multi-Tone DisturbanceHyland, D. C. / Davis, L. D. et al. | 1996
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