DocumentCode :
1801843
Title :
Orthogonal design-based evaluation for trajectory optimization algorithms
Author :
Dong Chunyun ; Cai Yuanli
Author_Institution :
Sch. of Electron. & Inf. Eng., Xi´an Jiaotong Univ., Xi´an, China
fYear :
2013
fDate :
26-28 July 2013
Firstpage :
8542
Lastpage :
8545
Abstract :
The analytic hierarchy process based performance evaluation for trajectories is analyzed in this paper, including the hierarchical evaluation system along with the ascent, cruise and descent phases, the judgment matrixes and the consistency check. The orthogonal design based evaluation for trajectory optimization algorithms is proposed, which can simulate the variable environment of flight and obtain multiple assessment results of optimization algorithms by selecting the trajectory optimization initial parameters as the orthogonal design factors reasonably. Moreover, we score and rank the optimization algorithms based on the quality ratio and Euclidean distance. The proposed assessment route is more objective and reasonable compared with the classical method. This approach is also very concise and easy to use. Preliminary simulation results indicate that the proposed technique can settle a proper order for different algorithms with a rational scoring agree with the engineering practical results effectively.
Keywords :
aerospace control; analytic hierarchy process; geometry; optimisation; trajectory control; Euclidean distance; analytic hierarchy process based performance evaluation; assessment route; hierarchical evaluation system; orthogonal design-based evaluation; quality ratio; trajectory optimization algorithms; Algorithm design and analysis; Analytic hierarchy process; Educational institutions; Electronic mail; Optimization; Performance evaluation; Trajectory; Analytic Hierarchy Process; Orthogonal design; Performance evaluation; Trajectory optimization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6640953
Link To Document :
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