International space station U.S. GN&C momentum manager controller design for shuttle thermal protection system repair

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 1, Issue , 2005, Pages 403-413

  Sims, Christopher R ^a,b  

^a BOEING COMPANY   (United States)

^b ISS GN and C Systems Integration   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GYROSCOPES; ORBITS; REPAIR; SPACE SHUTTLES;

ATTITUDE CONTROL; INTERNATIONAL SPACE STATION; ORBITER REPAIR MANOEUVER (ORM); REPAIR POSITION;

SPACE STATIONS;

EID: 29744435378     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-5854     Document Type: Conference Paper

References (3)

1. Harduvel, J, "Continuous momentum management of earth-oriented spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 6, 1992, pp. 1417-1426.
2. Boyd, S., El Ghaoui, L., Feron, E., and Balakrishnan, V., Linear Matrix Inequalities in System and Control Theory, SIAM, Philadelphia, 1994, Chaps. 7
3. Subramaniam, M., and Phillips, R.F. II, "SOMBAT: An Efficient Dynamics And Controls Analysis Tool For Large-Order Flexible Multibody Systems," Paper No. AAS03-603, Session 13 ISS, AAS/AIAA Astrodynamics Specialist Conference, Big Sky, MT, August 6, 2003.