Reusable launch vehicle control using linear-adaptive and subspace-stabilization techniques

Journal of Guidance Control and Dynamics

Volumn 24, Issue 2, 2001, Pages 278-286

  Tournes, C ^a   Johnson, C D ^b  

^a Davidson Enterprises LLC   (United States)

^b UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ALGORITHMS; AUTOMATIC PILOTS; COMMAND AND CONTROL SYSTEMS; COMPUTER SIMULATION; INVERSE PROBLEMS; LINEAR CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; PROBLEM SOLVING; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TRAJECTORIES;

ATTITUDE MODE; FLIGHT CONTROL LAW; REUSABLE LAUNCH VEHICLE; SUBSPACE-STABILIZATION TECHNIQUE;

FLIGHT DYNAMICS;

EID: 0035279498     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4710     Document Type: Article

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