Optimal Combination of Aerodynamic and Reaction Jet Control in a Vertical Launch Vehicle, M.Sc. Thesis Sharif University of Technology ; Nobahari, Hadi (Supervisor) ; Kashefi, Saeid (Co-Advisor)
Abstract
In this research, the design of control system has been studied for a special flying vehicle at whole of flight time. This flying vehicle is vertically launched and few time after launch its attitude changes to the desired attitude by a reaction jet control system, then the acceleration commands are tracked when the aerodynamic is activated. Design process includes attitude control system design in launch phase and aerodynamic control system design. Because of the existence of nonlinear and multi-variable dynamics in the flying vehicle and the presence of uncertainty and disturbance, combination of nonlinear, robust and adaptive methods are used in controller design process. Design of...
Cataloging briefOptimal Combination of Aerodynamic and Reaction Jet Control in a Vertical Launch Vehicle, M.Sc. Thesis Sharif University of Technology ; Nobahari, Hadi (Supervisor) ; Kashefi, Saeid (Co-Advisor)
Abstract
In this research, the design of control system has been studied for a special flying vehicle at whole of flight time. This flying vehicle is vertically launched and few time after launch its attitude changes to the desired attitude by a reaction jet control system, then the acceleration commands are tracked when the aerodynamic is activated. Design process includes attitude control system design in launch phase and aerodynamic control system design. Because of the existence of nonlinear and multi-variable dynamics in the flying vehicle and the presence of uncertainty and disturbance, combination of nonlinear, robust and adaptive methods are used in controller design process. Design of...
Find in contentBookmark |
|