Title :
Optimal Control and the Aircraft Radar Evasion Problem
Author :
Hussein, I.I. ; Zeitz, F.H. ; Bloch, A.M.
Author_Institution :
Worcester Polytech. Inst., Worcester
Abstract :
This paper considers the problem of optimal path planning for unmanned aerial vehicles in the presence of radar-guided surface-to-air missiles. The goal is to generate trajectories that ensure that the aerial vehicle visit a given set of way points while avoiding a given set of known locations of radar units. In this paper we first discuss the general radar evasion problem. Given that the aircraft equations of motion are nonholonomically constrained, the main mathematical tools used in this paper stem from nonlinear differential geometry. Hence, we introduce the constrained dynamic interpolation optimal control problem and state the optimality conditions. We then apply these conditions to the radar evasion problem. Finally, we provide numerical simulations that illustrate the ideas proposed in this paper.
Keywords :
aircraft; differential geometry; missile guidance; numerical analysis; optimal control; path planning; radar; aircraft equations; aircraft radar evasion problem; constrained dynamic interpolation optimal control problem; mathematical tools; nonlinear differential geometry; numerical simulations; optimal path planning; radar-guided surface-to-air missiles; unmanned aerial vehicles; Aerospace control; Airborne radar; Aircraft; Differential equations; Geometry; Missiles; Nonlinear equations; Optimal control; Path planning; Unmanned aerial vehicles;
Conference_Titel :
American Control Conference, 2007. ACC '07
Conference_Location :
New York, NY
Print_ISBN :
1-4244-0988-8
Electronic_ISBN :
0743-1619
DOI :
10.1109/ACC.2007.4282835