Control of approach and landing phase for reentry vehicle using fuzzy logic

Aerospace Science and Technology

Volumn 15, Issue 4, 2011, Pages 269-282

  Min, Chan Oh ^a   Lee, Dae Woo ^a   Cho, Kyeum Rae ^a   Jo, Sung Jin ^a   Yang, Jang Sik ^a   Lee, Won Boo ^b  

^a Pusan National University   (South Korea)

^b Shindong Co LTD   (South Korea)

Author keywords

Approach and landing; Fuzzy control; Mamdani method; Reentry

Indexed keywords

APPROACH AND LANDING; ATMOSPHERIC CONDITIONS; CENTER-OF-MASS; CONTROL SCHEMES; DEFUZZIFICATIONS; FUZZY INFERENCE SYSTEMS; FUZZY PD CONTROLLER; GEOMETRIC PARAMETER; GUIDANCE AND CONTROL; LANDING PHASE; MAMDANI; MAX-MIN METHOD; MONTE CARLO SIMULATION; RE-ENTRY VEHICLES; REFERENCE TRAJECTORIES; RELIABILITY AND ROBUSTNESS; ROBUST CONTROL SCHEME; WIND DISTURBANCE; WIND GUST;

COMPUTER SIMULATION; FUZZY CONTROL; FUZZY INFERENCE; FUZZY SYSTEMS; KNOWLEDGE BASED SYSTEMS; LANDING; MONTE CARLO METHODS; REENTRY; ROBUST CONTROL; SUPERSONIC AERODYNAMICS;

CONTROLLERS;

EID: 79955558846     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2010.07.006     Document Type: Article

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