Design of a missile autopilot using adaptive nonlinear dynamic inversion

Proceedings of the American Control Conference

Volumn 1, Issue , 2005, Pages 327-332

  Hindman, Rick ^a   Shell, William M ^a  

^a RAYTHEON COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; ERROR ANALYSIS; FLIGHT DYNAMICS; INTERPOLATION; NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION; PRODUCT DESIGN; ROBUSTNESS (CONTROL SYSTEMS);

ADAPTIVE NONLINEAR DYNAMIC INVERSION (ANDI); DYNAMIC INVERSION; MISSILE AUTOPILOT; PARAMETER VARIATION;

MISSILES;

EID: 23944439720     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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