Mixed programming control allocation for reusable launch vehicles using dynamic inverse calculating

Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics

Volumn 32, Issue 9, 2010, Pages

  He, Cheng Long ^a   Chen, Xin ^a   Yang, Yi Dong ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Control allocation; Dynamic inverse; Mixed programming; Reaction control system (RCS); Reusable launch vehicle (RLV)

Indexed keywords

AERODYNAMIC CONTROL; ANGULAR MOTIONS; CONTROL ALLOCATION; CONTROL EFFECTORS; CONTROL MOMENTS; FLIGHT ENVELOPE; INTEGER LINEAR PROGRAMMING; MIXED PROGRAMMING; MULTIPLE CONTROL EFFECTORS; OPTIMIZED CONTROL; REACTION CONTROL SYSTEM; REUSABLE LAUNCH VEHICLES; SIMULATION RESULT; THREE-AXIS;

CONTROL SURFACES; CONTROL THEORY; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; INTEGER PROGRAMMING; LAUNCH VEHICLES; MECHANICAL VARIABLES MEASUREMENT; OPTIMIZATION; REUSABILITY; REUSABLE ROCKETS; SURFACE REACTIONS; VEHICLES;

LAUNCHING;

EID: 77957938702     PISSN: 1001506X     EISSN: None     Source Type: Journal    
DOI: 10.3969/j.issn.1001-506X.2010.09.39     Document Type: Article

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