Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method

Acta Astronautica

Volumn 68, Issue 7-8, 2011, Pages 1176-1184

  Tian, Bailing ^a   Zong, Qun ^a  

^a TIANJIN UNIVERSITY   (China)

Author keywords

Guidance law; Indirect legendre pseudospectral method; Linear time varying; Reference trajectory

Indexed keywords

GUIDANCE LAWS; INITIAL-STATE UNCERTAINTIES; LEGENDRE; LEGENDRE PSEUDOSPECTRAL METHODS; LINEAR TIME VARYING; LINEAR TIME-VARYING SYSTEMS; MULTI-CONSTRAINTS; NON-LINEARITY; OPTIMAL GUIDANCE; PSEUDOSPECTRAL; RE-ENTRY VEHICLES; REAL TIME; REFERENCE TRAJECTORIES; REFERENCE TRAJECTORY; ROBUST STATE FEEDBACK; SIMULATION RESULT; STATE REGULATIONS;

FEEDBACK; FLIGHT SIMULATORS; LAWS AND LEGISLATION; NAVIGATION; REENTRY; TIME VARYING SYSTEMS; TRAJECTORIES;

STATE FEEDBACK;

EID: 79551533379     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2010.10.010     Document Type: Article

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