Coordinated control of a satellite-mounted manipulator with consideration of payload flexibility

Control Engineering Practice

Volumn 9, Issue 2, 2001, Pages 207-215

  Taniwaki, Shigemune ^a   Matunaga, Saburo ^b   Tsurumi, Shingo ^b   Ohkami, Yoshiaki ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Angular momentum; Experiment; Hoo control; Redundancy control; Robust control; Space robotics; Variable gain

Indexed keywords

COMPUTER SIMULATION; CONSTRAINT THEORY; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; MOTION CONTROL; MOTION PLANNING; ROBUSTNESS (CONTROL SYSTEMS);

ANGULAR MOMENTUM CONSTRAINTS (AMC); SATELLITE-MOUNTED MANIPULATORS;

MANIPULATORS;

SATELLITE;

EID: 0035071650     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(00)00099-X     Document Type: Article

References (8)

1. 2 control problems
2. Formulation of dynamical equations of motion
3. On-orbit robust control experiment of flexible spacecraft ETS-VI
4. Coordinated control of a satellite-mounted manipulator with compensation for inertial parameter variations (1st Report: A new method for coordinated control)
5. Coordinated control of spacecraft's attitude and its manipulator's (1st Report, Real-time estimation of the manipulator's reaction)
6. Coordinated control of a satellite-mounted manipulator with compensation for inertial parameter variations
7. Coordinated control experiment with a test bed imitated with a satellite-mounted manipulator