Computational Guidance Using Sparse Gauss-Hermite Quadrature Differential Dynamic Programming

被引：8

作者：

He, Shaoming ^{[1
]}

Shin, Hyo-Sang ^{[1
]}

Tsourdos, Antonios ^{[1
]}

机构：

[1] Cranfield Univ, Sch Aerosp Transport & Mfg, Cranfield MK43 0AL, Beds, England

来源：

IFAC PAPERSONLINE | 2019年 / 52卷 / 12期

关键词：

Computational guidance; Differential dynamic programming; Sparse Gauss-Hermite quadrature; Impact angle; Impact time; ANGLE; FILTER;

D O I：

10.1016/j.ifacol.2019.11.062

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper proposes a new computational guidance algorithm using differential dynamic programming and sparse Gauss-Hermite quadrature rule. By the application of sparse Gauss-Hermite quadrature rule, numerical differentiation in the calculation of Hessian matrices and gradients in differential dynamic programming is avoided. Based on the new differential dynamic programming approach developed, a three-dimensional computational algorithm is proposed to control the impact angle and impact time for an air-to-surface interceptor. Extensive numerical simulations are performed to show the effectiveness of the proposed approach. Copyright (C) 2019. The Authors. Published by Elsevier Ltd. All rights reserved.

引用

页码：13 / 18

页数：6

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