DocumentCode :
184339
Title :
Three-dimensional aircraft path planning based on nonconvex quadratic optimization
Author :
Ran Dai
Author_Institution :
Aerosp. Eng. Dept., Iowa State Univ., Ames, IA, USA
fYear :
2014
fDate :
4-6 June 2014
Firstpage :
4561
Lastpage :
4566
Abstract :
In this paper, we examine the three-dimensional aircraft path planning problems under field-of-view constraints using a nonconvex quadratic optimization method. The aircraft is assumed to be flying at constant speed with small angle of attack. We focus on determining the attitude of the aircraft when planning the optimal paths. Under this venue, the aircraft kinematics are expressed as quadratic functions in terms of unit quaternions and the path planning problem is reformulated as a general quadratically constrained quadratic programming (QCQP) problem. A semidefinite programming method is then applied to relax the nonconvex QCQP problem to obtain the bounds on the optimal value. Subsequently, an iterative rank minimization approach is proposed to find the optimal solution. Simulation results for planned paths using the proposed method are presented and compared with those obtained from the other method.
Keywords :
aircraft; concave programming; path planning; quadratic programming; 3D aircraft path planning; aircraft kinematics; iterative rank minimization; nonconvex QCQP problem; nonconvex quadratic optimization; optimal paths; optimal solution; optimal value; quadratic functions; quadratically constrained quadratic programming; semidefinite programming method; unit quaternions; Aircraft; Eigenvalues and eigenfunctions; Kinematics; Path planning; Quaternions; Symmetric matrices; Vectors; Nonconvex Quadratically Constrained Quadratic Programming; Path Planning; Semidefinite Programming; Unit Quaternion;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2014
Conference_Location :
Portland, OR
ISSN :
0743-1619
Print_ISBN :
978-1-4799-3272-6
Type :
conf
DOI :
10.1109/ACC.2014.6859054
Filename :
6859054
Link To Document :
بازگشت