Variable structure near space vehicle control characteristics of large flight envelope

Yuhang Xuebao/Journal of Astronautics

Volumn 30, Issue 2, 2009, Pages 543-549

  Zhang, Jun ^a   Jiang, Chang Sheng ^a   Fang, Wei ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Control characteristics; Large flight envelop; Near space vehicle; Variable structure

Indexed keywords

AERODYNAMIC COEFFICIENTS; CONTROL CHARACTERISTICS; COUPLING CHARACTERISTIC; DYNAMIC SYSTEMS; FLIGHT CONDITIONS; FLIGHT ENVELOP; FLIGHT ENVELOPE; GENERIC HYPERSONIC VEHICLES; MODE-BASED; NEAR-SPACE VEHICLES; SIMULATION RESULT; TIGHT COUPLING; TIME VARYING; VARIABLE STRUCTURES;

CONTROL SYSTEM SYNTHESIS; DYNAMICAL SYSTEMS; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; GAS DYNAMICS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; MACH NUMBER;

VEHICLES;

EID: 70249099182     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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