Reusable Launch Vehicle guidance and control using subspace stabilization control techniques

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 183-191

  Toumes, C ^a   Johnson, C D ^b  

^a AIAA   (United States)

^b UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; AUTOMATIC PILOTS; FLIGHT CONTROL SYSTEMS; LAUNCH VEHICLES; REUSABILITY; REUSABLE ROCKETS; ROBUST CONTROL; WIND TUNNELS;

CONTROL ARCHITECTURE; DISTURBANCE ACCOMMODATION; NONLINEAR TECHNIQUES; PROPOSED ARCHITECTURES; REUSABLE LAUNCH VEHICLES; ROBUST CONTROL TECHNIQUES; STABILIZATION CONTROL; STABILIZATION TECHNIQUES;

STABILIZATION;

EID: 84959177546     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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