TY - JOUR
T1 - Study of multi-objective trajectory optimization based on physical programming
AU - Liu, Li
AU - Xing, Chao
AU - Long, Teng
PY - 2013/4
Y1 - 2013/4
N2 - The weighted summary method (WSM) is widely adopted in the multi-objective trajectory optimization. However, it is rather difficult to obtain the non-convex Pareto non-inferior solutions by using WSM, and weights subjectively determined by users are usually inappropriate. To overcome the disadvantages above, the physical programming method is introduced and the model based on physical programming is presented for multi-objective trajectory optimization. The procedure of multi-objective trajectory optimization using physical programming was analyzed in detail and the advantages of proposed method were also pointed out. The pullout segment trajectory of a missile was optimized respectively by using three methods: WSM, optimal control theory method and the physical programming method. Through comparison of the optimization results, it is demonstrated that physical programming method has the advantages over other two methods. It is more efficient and robust, and is insensitive to initial value. It could achieve better optimization results. In addition, it has the ability of achieving the non-convex Pareto non-inferior solution. Thus, the physical programming method proposed in this article is proved to be quite practical in multi-objective trajectory optimization.
AB - The weighted summary method (WSM) is widely adopted in the multi-objective trajectory optimization. However, it is rather difficult to obtain the non-convex Pareto non-inferior solutions by using WSM, and weights subjectively determined by users are usually inappropriate. To overcome the disadvantages above, the physical programming method is introduced and the model based on physical programming is presented for multi-objective trajectory optimization. The procedure of multi-objective trajectory optimization using physical programming was analyzed in detail and the advantages of proposed method were also pointed out. The pullout segment trajectory of a missile was optimized respectively by using three methods: WSM, optimal control theory method and the physical programming method. Through comparison of the optimization results, it is demonstrated that physical programming method has the advantages over other two methods. It is more efficient and robust, and is insensitive to initial value. It could achieve better optimization results. In addition, it has the ability of achieving the non-convex Pareto non-inferior solution. Thus, the physical programming method proposed in this article is proved to be quite practical in multi-objective trajectory optimization.
KW - Multi-objective optimization
KW - Optimal control
KW - Physical programming
KW - Trajectory
KW - Weighted summary method
UR - http://www.scopus.com/inward/record.url?scp=84878497492&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:84878497492
SN - 1001-0645
VL - 33
SP - 357
EP - 362
JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
JF - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
IS - 4
ER -