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http://dx.doi.org/10.3795/KSME-A.2009.33.9.922

Waypoints Guidance of the Nonlinear Helicopter using the SDRE Technique  

Kim, Min-Jae (건국대학교 대학원 항공우주정보시스템공학과)
Yang, Chang-Deok (건국대학교 대학원 항공우주정보시스템공학과)
Hong, Ji-Seung (건국대학교 대학원 항공우주정보시스템공학과)
Kim, Chang-Joo (건국대학교 항공우주정보시스템공학과)
Publication Information
Transactions of the Korean Society of Mechanical Engineers A / v.33, no.9, 2009 , pp. 922-929 More about this Journal
Abstract
This paper deals with the State-Dependent Riccati Equation (SDRE) Technique for the design of helicopter nonlinear waypoint guidance controller. To generate the flight guidance through multiple waypoints, we use the trigonometric spline. The controller design and its validation is based upon a level 2 simulation helicopter model and the designed SDRE controller is applied to the trajectory tracking problems. To validate the designed SDRE controller, the simulation environment of high fidelity helicopter model is developed using three independent computers. This paper focuses on the validation the present SDRE controller through the helicopter waypoint guidance simulation.
Keywords
Helicopter Flight Control; SDRE, Trajectory Generation; Waypoint Guidance;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
Times Cited By SCOPUS : 0
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