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Research article

First published 2012-12

Extended state observer-based robust pitch autopilot design for tactical missiles

A A Godbole, T R Libin, S E Talole

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

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Research article

First published 2014-2

Design and comparison of autopilots of an air-to-surface antitank missile and its terminal guidance study

Celâl Ada, Ayhan Kural

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

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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 2017-8

Distributed composite autopilot design for bank-to-turn missiles with optimized tracking based on disturbance observers

Jun Yang, Chao Wu, Shihua Li

Transactions of the Institute of Measurement and Control

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Research article

First published 2012-1

Robust autopilot design of uncertain bank-to-turn missiles using state-space disturbance observers

J Yang, W-H Chen, S Li

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

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Research article

First published 2019-4

A 3D pitch and impact-angle constrained guidance scheme

S Aditya Varma, Mangal Kothari

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

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Research article

First published 2015-7

Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach

Yao Zhao, Jiabin Chen, Yongzhi Sheng

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

Open access

Research article

First published 2019-11

Partial integrated guidance and control design for supersonic missile based on disturbance rejection

Minnan Piao, Mingwei Sun, Jian Huang [...]

Measurement and Control

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Research article

First published 2016-10

Generalized extended state observer-based H ∞ control design for a missile longitudinal autopilot

Yi Dong, Jian Li, Tong Li

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

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