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Research article

First published 2016

Suboptimal mid-course guidance algorithm for accelerating missiles

Min-Guk Seo, Min-Jea Tahk

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

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Research article

First published 2005-2

Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile

L Bruyere, A Tsourdos, B A White

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

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Research article

First published 2012-8

Missile acceleration controller design using proportional–integral and non-linear dynamic control design method

S-H Kim, M-J Tahk

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

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Research article

First published 2006-08

Accelerating Missile Threat Simulations Using Personal Computer Graphics Cards

Sean A. Jeffers, Rusty O. Baldwin, Barry E. Mullins

SIMULATION

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Research article

First published 2022-12

Gravity-compensated guidance for impact-angle interception of a moving target

Hyeong-Geun Kim, Jun-Yong Lee, Pyojin Kim

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

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Research article

First published 2016-2

Adaptive nonsingular terminal sliding mode cooperative guidance law in active defense scenario

Xinguang Zou, Di Zhou, Runle Du [...]

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

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Research article

First published 2019-1

Simultaneous attack strategy against a maneuvering target with unknown acceleration

Zilun Hu, Jianying Yang

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

Open access

Research article

First published 2022-11

Dynamic interception point guidance algorithm based on particle swarm optimization

Yi-Wei Chen

Measurement and Control

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Research article

First published 2006-5

Hybrid guidance law for interception of ballistic targets

C-L Lin, K-M Chen, M-T Wu [...]

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

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