Performance Evaluation of Guidance and Control System Based on Improved Latin Hypercube

doi:10.16182/j.issn1004731x.joss.201710016

Abstract

Abstract: Aiming at the low efficiency and the poor space-filling property in the aircraft performance evaluation combined with simulation experiment, a novel aircraft performance evaluation method based on the improved LHD (Latin hypercube designs) was investigated. The six-DOF (Degree of Freedom) rigid aircraft model was built. Considering the characteristic of BTT (bank-to-turn) vehicle in dive phase, the performance evaluation index system of its guidance and control system was set up. The optimal LHD was applied to the performance evaluation of the aircraft guidance and control system. The improved algorithm can quickly construct a good design of experiments given a limited computational resource. The instance of performance evaluation verifies that the proposed approach is effective and feasible.

Key words: experimental design, guidance and control system, performance evaluation, improved Latin hypercube design

CLC Number:

TJ765

Zhang Denghui, Chao Tao, Wang Songyan, Ma Ping. Performance Evaluation of Guidance and Control System Based on Improved Latin Hypercube[J]. Journal of System Simulation, 2017, 29(10): 2345-2352.

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