Adaptive output feedback tracking control of spacecraft formation

International Journal of Robust and Nonlinear Control

Volumn 12, Issue 2-3, 2002, Pages 117-139

  Wong, Hong ^a   Kapila, Vikram ^a   Sparks, Andrew G ^b  

^a POLYTECHNIC UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Adaptive control; Output feedback; Spacecraft formation flying

Indexed keywords

ALGORITHMS; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DYNAMICS; FEEDBACK CONTROL; MATHEMATICAL MODELS; MOTION CONTROL; PARAMETER ESTIMATION; POSITION CONTROL; SPACECRAFT; TRACKING (POSITION);

CONSTRAINT EQUATION; CONTROL LAW; CONVERGENCE OF DISTURBANCE PARAMETER ESTIMATES; ELLIPTICAL ORBIT; INITIAL CONDITION; LAGRANGIAN DERIVATION; OUTPUT FEEDBACK; SPACECRAFT FORMATION FLYING;

ADAPTIVE CONTROL SYSTEMS;

EID: 0036465645     PISSN: 10498923     EISSN: None     Source Type: Journal    
DOI: 10.1002/rnc.679     Document Type: Article

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