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A nonlinear impact-angle guidance law

Mandar Bhanudas Kamalaskar (Department of Aerospace, Indian Institute of Technology Kharagpur, Kharagpur, India)
S. Aditya Varma (Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, India)
Mangal Kothari (Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, India)

International Journal of Intelligent Unmanned Systems

ISSN: 2049-6427

Article publication date: 19 April 2017

145

Abstract

Purpose

The purpose of this paper is to propose a new nonlinear guidance law to satisfy terminal impact-angle constraints against a stationary target in every possible planar surface-to-surface engagement scenario. The proposed guidance scheme is developed based on the geometry of a circular arc trajectory. The proposed guidance scheme is developed based on the geometry of circular arc trajectory. This trajectory is calculated based on the terminal impact angle and target range. The efficacy of the proposed guidance scheme is demonstrated through numerical simulations. The proposed scheme is compared with existing guidance schemes and relevant analysis is provided.

Design/methodology/approach

The paper develops a new nonlinear guidance law to satisfy terminal impact-angle constraints against a stationary target in every possible planar surface-to-surface engagement scenario. The proposed guidance scheme is developed based on the geometry of a circular arc trajectory. This guidance scheme is further extended to moving targets.

Findings

The proposed guidance intercepts a stationary target with a smooth lateral acceleration command, which is desirable for realistic implementation. The efficacy of the approach is demonstrated through numerical simulation. A comparative study with the existing algorithm is presented and it is shown that the proposed algorithm is better on many counts.

Originality/value

There are many approach exists in the literature for impact-angle guidance laws. The paper proposes a computationally efficient guidance law using geometric and kinematic properties. As the approach produces smooth command, it has a practical relevance. A comparative study shows superiority on some counts (miss distance, flight time, smoothness).

Keywords

Citation

Kamalaskar, M.B., Varma, S.A. and Kothari, M. (2017), "A nonlinear impact-angle guidance law", International Journal of Intelligent Unmanned Systems, Vol. 5 No. 2/3, pp. 46-62. https://doi.org/10.1108/IJIUS-03-2017-0003

Publisher

:

Emerald Publishing Limited

Copyright © 2017, Emerald Publishing Limited

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