Control allocation for an over-actuated Satellite Launch Vehicle

Aerospace Science and Technology

Volumn 28, Issue 1, 2013, Pages 56-71

  Kishore, W C Arun ^a   Dasgupta, Santanu ^b   Ray, Gosaidas ^c   Sen, Siddhartha ^c  

^a Department of Mechanical Engineering   (India)

^b Mohandas College of Engineering and Technology Thiruvananthapuram   (India)

^c INDIAN INSTITUTE OF TECHNOLOGY   (India)

Author keywords

Attitude control; Control allocation; Disturbance rejection; Linear Matrix Inequality (LMI); Partial state feedback control; Pole placement control; Satellite Launch Vehicle

Indexed keywords

ALLOCATION ALGORITHM; COMBINED ALGORITHMS; CONTROL ALLOCATION; LINEAR MATRIX INEQUALITY APPROACH; PARTIAL STATE FEEDBACK; POLE-PLACEMENT CONTROLS; SATELLITE LAUNCH VEHICLES; STATE FEEDBACK CONTROLLER;

ACTUATORS; ALGORITHMS; ALIGNMENT; ATTITUDE CONTROL; DISTURBANCE REJECTION; FEEDBACK CONTROL; LINEAR MATRIX INEQUALITIES; RIGID STRUCTURES; STATE FEEDBACK;

CONTROLLERS;

EID: 84878866121     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2012.10.004     Document Type: Article

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