Dynamic inversion via state dependent riccati equation approach: Application to flight vehicles

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Shankar, Praveen ^a   Yedavalli, Rama K ^a   Doman, David B ^b  

^a OHIO STATE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AND FILTERS; DESIGN METHOD; DYNAMIC INVERSION; FLIGHT VEHICLES; NON-LINEAR CONTROLLERS; PERFORMANCE CHARACTERISTICS; STATE-DEPENDENT ALGEBRAIC RICCATI EQUATIONS; STATE-DEPENDENT RICCATI EQUATION;

CONTROL THEORY; RICCATI EQUATIONS;

FLIGHT CONTROL SYSTEMS;

EID: 84896693554     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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