Optimal control design using an H2 method for the glovebox integrated microgravity isolation technology (g-LIMIT)

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Calhoun, Philip C ^a   Hampton, R David ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b UNITED STATES MILITARY ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; ACTUATORS; MAGNETIC ACTUATORS; MICROGRAVITY; MICROGRAVITY PROCESSING; NASA; SPACE FLIGHT; SPACE STATIONS;

ACCELERATION ENVIRONMENTS; ISOLATION TECHNOLOGY; LINEAR OPTIMAL CONTROLS; MICRO-GRAVITY SCIENCE; OPTIMAL CONTROL DESIGN; PAYLOAD ACCELERATIONS; RELATIVE ORIENTATION; VIBRATION ISOLATIONS;

CONTROLLERS;

EID: 85086618731     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-5020     Document Type: Conference Paper

References (3)

1. Hampton, R.D., Calhoun P.C., Whorton, M.K., "Glovebox Integrated Microgravity Isolation Technology (g-LIMIT): A Linearized State-Space Model", NASA TM-2002-211674, July 2002.
2. Whorton, M. S., et al, "Design Definition Document (DDD) For Glovebox Integrated Micrograv-ity Isolation Technology (g-LIMIT) Characterization Test", g-LIMIT-DOC-0001, NASA Marshall Space Flight Center, September 30, 1999.
3. Hampton, R.D., Whorton, M.S., "Design-Filter Selection for H2 Control of Microgravity Isolation Systems: A Single-Degree-of-Freedom Case Study", AIAA-2000-3955, August 2000. Submitted to the Journal of Guidance, Control, and Dynamics, September 2000.