Use of guidance and control test cases to verify spacecraft attitude control system design

Advances in the Astronautical Sciences

Volumn 112 I, Issue , 2002, Pages 317-337

  Chang, Larry ^a   Brown, Jay M ^a   Barltrop, Kevin J ^a   Lee, Allan Y ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; FLIGHT DYNAMICS; INTERPLANETARY FLIGHT; ORBITS; POSITION CONTROL; PROPELLANTS; TELEMETERING;

CASSINI SPACECRAFT; CONTROL TESTING; DEEP SPACE MISSION; FLIGHT TELEMETRY; SPACECRAFT ATTITUDE CONTROL;

INTERPLANETARY SPACECRAFT;

EID: 0036919270     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Jaffe, L. and Herrell, L., "Cassini Huygens Science Instruments, Spacecraft, and Mission," Journal of Spacecraft and Rockets, Vol. 34, No. 4, 1997, pp. 509-521.
2. Wong, E. and Breckenridge, W., "An Attitude Control Design for the Cassini Spacecraft," Proceedings of the AIAA Guidance, Navigation, and Control Conference, Washington D.C., 1995, pp. 931-945.
3. Wette, M., et al., "Flight Software Development System User's Guide," version 2.08, October 7, 1999. Jet Propulsion Laboratory, California Institute of Technology.
4. Boehmer, R. "AACS TCM 10 Final Report," IOM SCO-99-077, October 19, 1999. Jet Propulsion Laboratory, California Institute of Technology.
5. Lee, A. "Cassini Orbiter Functional Requirements Book: Accuracy Requirements and System Capabilities," CAS 3-170, Revision D, November 7, 1997. Jet Propulsion Laboratory, California Institute of Technology.