Feedback guidance scheme for orbital rendezvous

Journal of the Astronautical Sciences

Volumn 47, Issue 3-4, 1999, Pages 229-237

  Kluever, Craig A ^a   Tanck, Greg S ^b  

^a University of Missouri   (United States)

^b UNIVERSITY OF MISSOURI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONVERGENCE OF NUMERICAL METHODS; ELECTRIC PROPULSION; OPTIMIZATION; ORBITS; PROBLEM SOLVING; SPACECRAFT PROPULSION; FEEDBACK; SPACE FLIGHT; SPACE STATIONS;

LINEAR QUADRATIC REGULATORS;

SPACE RENDEZVOUS;

CLOSED LOOP RESPONSE; ELECTRIC PROPULSION THRUSTERS; IMPULSIVE VELOCITY; LINEAR QUADRATIC REGULATOR; OPTIMAL WEIGHTING; ORBITAL RENDEZVOUS; PARAMETER OPTIMIZATION METHODS; RAPID CONVERGENCE;

EID: 0033156136     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (12)

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