Networked flexible spacecraft attitude maneuver based on adaptive fuzzy sliding mode control

Acta Astronautica

Volumn 65, Issue 11-12, 2009, Pages 1561-1570

  Dong, Chaoyang ^a   Xu, Lijie ^a   Chen, Yu ^a   Wang, Qing ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Adaptive fuzzy control; Flexible spacecraft attitude control; Networked control systems (NCS); Sliding mode control

Indexed keywords

ADAPTIVE FUZZY CONTROL; ADAPTIVE FUZZY SLIDING-MODE CONTROLS; ADAPTIVE FUZZY SYSTEM; ATTITUDE STABILIZATION; ELASTIC VIBRATION; FLEXIBLE SPACECRAFT ATTITUDE CONTROL; FLEXIBLE SPACECRAFTS; HIGH-PRECISION; LYAPUNOV STABILITY THEOREM; NETWORK-INDUCED DELAYS; NETWORKED CONTROL SYSTEMS (NCS); NON-LINEAR DYNAMICS; NONLINEAR PREDICTORS; SIMULATION RESULT; STRONG COUPLING; SYSTEM UNCERTAINTIES; SYSTEM-TRACKING STABILITY; UNCERTAIN PARAMETERS;

ADAPTIVE ALGORITHMS; ATTITUDE CONTROL; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; FUZZY CONTROL; FUZZY LOGIC; NAVIGATION; SLIDING MODE CONTROL; SPACECRAFT; SPATIAL VARIABLES CONTROL; STABILIZATION; SYSTEM STABILITY; UNCERTAINTY ANALYSIS;

ADAPTIVE CONTROL SYSTEMS;

EID: 70349766936     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2009.04.004     Document Type: Article

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