DocumentCode :
2431846
Title :
Optimal vertical maneuvers of the aircraft with thrust vectoring in the rigid body model
Author :
Takano, Hiroyuki ; Wada, Hidesuke ; Yamasaki, Takeshi ; Baba, Yoriaki
Author_Institution :
Nat. Defense Acad., Yokosuka
fYear :
2007
fDate :
17-20 Oct. 2007
Firstpage :
2100
Lastpage :
2103
Abstract :
Maneuverability of aircraft, particularly high-performance aircraft, has been improved remarkably, which include the poststall maneuverability and the thrust vectoring. However, the performance of the aircraft is shown well only when the aircraft carry out the best maneuvers. In this paper, we try to optimize the vertical loop of the aircraft with poststall maneuverability and thrust vectoring control in the rigid body model. We formulate the trajectory optimization as a nonlinear programming problem and analyzed numerically. The optimal solutions we obtained show better performance than those of ordinary aircraft, although poststall flights in the low speed seem difficult and dangerous. Thus, those maneuvers might be good for unmanned aerial vehicles.
Keywords :
aircraft control; motion control; nonlinear programming; optimal control; position control; aircraft maneuverability; nonlinear programming problem; optimal vertical maneuvers; poststall maneuverability; rigid body model; thrust vectoring control; trajectory optimization; unmanned aerial vehicles; vertical loop; Aerospace control; Aircraft propulsion; Automatic control; Automation; Boundary conditions; Control system synthesis; Equations; Navigation; Optimal control; Unmanned aerial vehicles; Aircraft; Guidance and Control; Poststall; Trajectory Optimization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems, 2007. ICCAS '07. International Conference on
Conference_Location :
Seoul
Print_ISBN :
978-89-950038-6-2
Electronic_ISBN :
978-89-950038-6-2
Type :
conf
DOI :
10.1109/ICCAS.2007.4406676
Filename :
4406676
Link To Document :
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