ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Analysis of a Two-Gain Guidance Law against Nonmaneuvering Moving Targets

Sharma, YR and Ratnoo, A (2021) Analysis of a Two-Gain Guidance Law against Nonmaneuvering Moving Targets. In: IEEE Transactions on Aerospace and Electronic Systems, 57 (6). pp. 4002-4016.

[img] PDF
iee_tra_aer_ele_sys_57-06_4002-4016_2021.pdf - Published Version
Restricted to Registered users only

Download (2MB) | Request a copy
Official URL: https://doi.org/10.1109/TAES.2021.3088497

Abstract

In this article, a novel two-gain guidance law is investigated for the problem of impact-angle controlled interception of nonmaneuvering moving targets considering seeker field-of-view limit. The problem considers a planar surface-to-surface engagement scenario where the target moves either along the initial line-of-sight or opposite to that. Imposing a desired impact-angle and maximum field-of-view limit of the seeker as constraints, closed-form expressions of the two guidance gains are deduced. Feasible solutions guaranteeing a bounded lateral acceleration profile are obtained as expressed in maximum look-angle-impact-angle, and maximum look angle-target speed design spaces. Extensive numerical simulations are carried out showing the efficacy of the proposed guidance method in intercepting moving targets without violating the seeker field-of-view limit. In contrast to existing guidance methods, the proposed work presents a simpler solution which does not rely on bias addition, switching, or iterative routines. © 1965-2011 IEEE.

Item Type: Journal Article
Publication: IEEE Transactions on Aerospace and Electronic Systems
Publisher: Institute of Electrical and Electronics Engineers Inc.
Additional Information: The copyright for this article belongs to Institute of Electrical and Electronics Engineers Inc.
Keywords: Electronic guidance systems; Iterative methods, Angle control; Field of views; Field-of-view constraint; Gain-guidance; Impact angles; Impact-angle control; Moving target interception; Moving targets; Trajectory shaping; Trajectory shaping guidance, Numerical methods
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 06 Jan 2022 11:36
Last Modified: 06 Jan 2022 11:36
URI: http://eprints.iisc.ac.in/id/eprint/70813

Actions (login required)

View Item View Item