Optimal guidance law design for three-dimensional trajectory tracking of missiles based on fixed-gain disturbance observer-Reference-Cited by-同舟云学术

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Optimal guidance law design for three-dimensional trajectory tracking of missiles based on fixed-gain disturbance observer

Published:2023-12 Issue: Volume:143 Page:298-312
ISSN:0019-0578
Container-title:ISA Transactions
language:en
Short-container-title:ISA Transactions

Author:

Zhang Ke,Zhang Zhenlin^ORCID,Han Zhiguo

Funder

Fundamental Research Funds for the Central Universities

Aviation Engine Innovation Center of National Defense Science Technology and Industry

National Natural Science Foundation of China

Chinese Aeronautical Establishment

Publisher

Elsevier BV

Subject

Applied Mathematics,Control and Systems Engineering,Electrical and Electronic Engineering,Computer Science Applications,Instrumentation

Reference36 articles.

1. Suboptimal midcourse guidance of interceptors for high-speed targets with alignment angle constraint;Dwivedi;J Guid Control Dyn,2011

2. Adaptive sliding mode guidance law for missile with adjustable flight speed;Hua;Electr Opt Control,2022

3. Optimal tracking guidance for aeroassisted spacecraft reconnaissance mission based on receding horizon control;Chai;IEEE Trans Aerosp Electron Syst,2018

4. Path-following control for fixed-wing unmanned aerial vehicles based on a virtual target;Zhang;Proc Inst Mech Eng G,2014

5. Augmented L1 adaptive tracking control of quad-rotor unmanned aircrafts;Zuo;IEEE Trans Aerosp Electron Syst,2014

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