Quaternion observer-based model-independent attitude tracking control of spacecraft

Journal of Guidance, Control, and Dynamics

Volumn 32, Issue 5, 2009, Pages 1476-1482

  Song, Y D ^a   Cai, Wenchuan ^b,c  

^a BEIJING JIAOTONG UNIVERSITY   (China)

^b NORTH CAROLINA A AND T STATE UNIVERSITY   (United States)

^c Electrical and Computer Engineering

Author keywords

[No Author keywords available]

Indexed keywords

NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION; RIGID STRUCTURES; TRACKING (POSITION); UNCERTAINTY ANALYSIS;

ATTITUDE TRACKING CONTROL; CONTROL STRATEGIES; EXTERNAL DISTURBANCES; MODEL INDEPENDENT; RIGID BODY SPACECRAFT; SEPARATION PROPERTY; STABILITY ANALYSIS; SYSTEM DYNAMIC MODELS;

NAVIGATION;

EID: 72149117109     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.43029     Document Type: Article

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