Practical Aspects of Optimal Midcourse Guidance For Air-to-air Engagement

被引：4

作者：

Majumder, S. B. ^{[1
]}

Basha, S. M. ^{[1
]}

Tiwari, P. K. ^{[1
]}

Prasad, D. B. N. ^{[1
]}

Sarkar, A. K. ^{[1
]}

机构：

[1] DRDL, Hyderabad 500058, Andhra Pradesh, India

来源：

IFAC PAPERSONLINE | 2016年 / 49卷 / 01期

关键词：

Singular Perturbation; Midcourse Guidance; Air-to-Air Engagement;

D O I：

10.1016/j.ifacol.2016.03.119

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Singular control can be used to be solve midcourse guidance problem in real time for air-to-air engagement. optimal solution. The objective function can be as simple as minimizing flight tune. This near optimal solution works excellently in real time to enhance missile kinematic range compared to same obtained using classical PN guidance law in air-to-air engagement,. Here both shooter aircraft and target aircraft kinematics varies dynamically. Implementation of such guidance law can give sonic practical problem due to nonlinearities in aerodynamic data, atmospheric model and maneuvering target models. In this paper these practical problems have been highlighted and method of solution in high fidelity six degrees of freedom simulation environment has been discussed. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.

引用

页码：591 / 596

页数：6

共 12 条

[1]

[Anonymous], 1969, Applied Optimal Control

[2]

Basha S. M., 2015, MISSION REV ASTRA RE

[3] ADVANCED MIDCOURSE GUIDANCE FOR AIR-TO-AIR MISSILES [J].