Reentry guidance law design for RLV based on predictor-corrector method

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 35, Issue 11, 2009, Pages 1344-1348

  Li, Huifeng ^a   Xie, Ling ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Path constraint; Predictor corrector; QEGC; Reentry; RLV

Indexed keywords

BANK ANGLE PROFILE; DYNAMIC EQUATIONS; DYNAMIC PRESSURES; GUIDANCE LAWS; HEAT RATE; HIGH ROBUSTNESS; INITIAL STATE; MONTE CARLO SIMULATION; NORMAL LOADS; PATH CONSTRAINT; PREDICTOR CORRECTOR; PREDICTOR-CORRECTOR METHODS; QUASI-EQUILIBRIUM; RE-ENTRY GUIDANCE; REUSABLE LAUNCH VEHICLES; SIMULATION RESULT;

COMPUTER SIMULATION; LAUNCHING; MONTE CARLO METHODS;

REUSABLE ROCKETS;

EID: 72449121393     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (7)

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