Pseudo-Spectral MPSP-Based Unified Midcourse and Terminal Guidance for Reentry Targets

A unified optimal guidance scheme is presented in this article for both midcourse and terminal phases combined. It minimizes the total deceleration resulting in enhanced range and/or higher impact velocity, while satisfying the terminal constraints on impact angle and miss distance. State-dependent...

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Bibliographic Details
Published in:	IEEE transactions on aerospace and electronic systems Vol. 59; no. 4; pp. 3982 - 3994
Main Authors:	Sharma, Prayag, Kumar, Prem, Padhi, Radhakant
Format:	Journal Article
Language:	English
Published:	New York IEEE 01.08.2023 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects:	Aerodynamics Angle-constrained guidance Cost function Deceleration Drag Force Impact velocity midcourse guidance minimum acceleration guidance Miss distance Missiles model predictive static programming (MPSP) guidance optimal guidance Philosophical considerations Solid modeling Terminal constraints Terminal guidance Three-dimensional displays
ISSN:	0018-9251, 1557-9603
Online Access:	Get full text
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