New nonlinear control technique for ascent phase of reusable launch vehicles

Journal of Guidance, Control, and Dynamics

Volumn 27, Issue 6, 2004, Pages 938-948

  Drake, David ^a,b   Xin, Ming ^a,b   Balakrishnair, S N ^a,b  

^a MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY   (United States)

^b Department of Mechanical Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL EQUIPMENT; DEGREES OF FREEDOM (MECHANICS); HAMILTONIANS; LAGRANGE MULTIPLIERS; NONLINEAR CONTROL SYSTEMS; PERTURBATION TECHNIQUES; THREE TERM CONTROL SYSTEMS; VECTORS;

EULER ANGLE VECTOR; MACH NUMBER; REUSABLE LAUNCH VEHICLES;

VEHICLES;

EID: 9944259105     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9058     Document Type: Article

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