Nonlinear receding-horizon state estimation by real-time optimization technique

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 4, 1996, Pages 863-870

  Ohtsuka, Toshiyuki ^a,b,c   Fujii, Hironori A ^b,c,d,e,f,g  

^a UNIVERSITY OF TSUKUBA   (Japan)

^b TOKYO METROPOLITAN UNIVERSITY   (Japan)

^c University of Tsukuba ^*

^d KYOTO UNIVERSITY   (Japan)

^e Res Grp Contr Flexible Space S   (Japan)

^f American Astronautical Society

^g Can Aeronautics and Space Institute

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; APPROXIMATION THEORY; COMPUTER SIMULATION; DIGITAL COMPUTERS; FEEDBACK CONTROL; MODELS; NONLINEAR SYSTEMS; OPTIMIZATION; REAL TIME SYSTEMS;

NONLINEAR SPACE VEHICLE; RECEDING HORIZON PERFORMANCE INDEX; STABILIZED CONTINUATION METHOD;

STATE ESTIMATION;

EID: 0030194070     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21711     Document Type: Article

References (11)

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