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Research article

First published 2018-7

Super-twisting integral-sliding-mode guidance law considering autopilot dynamics

Kezi Meng, Di Zhou

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Open access

Research article

First published 2017-11

Command filtered back-stepping missile integrated guidance and autopilot based on extended state observer

Liang Wang, Weihua Zhang, Donghui Wang [...]

Advances in Mechanical Engineering

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Research article

First published 2016-1

Integrated versus two-loop guidance-autopilot for a dual control missile with high-order aerodynamic model

FB Ibarrondo, P Sanz-Aránguez

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2013-8

Composite guidance laws based on sliding mode control with impact angle constraint and autopilot lag

Zhenxing Zhang, Shihua Li, Sheng Luo

Transactions of the Institute of Measurement and Control

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Research article

First published 2019-6

Two composite guidance laws based on the backstepping control and disturbance observers with autopilot lag

Chaoyuan Man, Zhenxing Zhang, Shihua Li

Transactions of the Institute of Measurement and Control

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Research article

First published 2013-2

Sliding-mode-based contour-following controller for guidance and autopilot systems of launch vehicles

Fu-Kuang Yeh

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2023-7

An event-triggered distributed cooperative guidance law for simultaneous attack with autopilot lag consideration

Jinpeng Zhai, Jianying Yang

Transactions of the Institute of Measurement and Control

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Research article

First published 1996-4

Missile autopilot controller design using state transformations and optimal LQR techniques

Campbell Jones

Transactions of the Institute of Measurement and Control

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Research article

First published 2013-7

A novel robust proportional navigation guidance law design for missile considering autopilot dynamic

Seyyed Sajjad Moosapour, Ghasem Alizadeh, Sohrab Khanmohammadi [...]

Transactions of the Institute of Measurement and Control

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Research article

First published 2009-3

Approximate closed-form solutions of realistic true proportional navigation guidance using the Adomian decomposition method

T Garai, S Mukhopadhyay, D Ghose

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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