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Research article

First published 2013-3

An algorithm for selecting optimal controls to determine the estimators of the coefficients of a mathematical model for the dynamics of a self-propelled anti-aircraft missile system

Zbigniew Koruba, Izabela Krzysztofik

Proceedings of the Institution of Mechanical Engineers,Part K: Journal of Multi-body Dynamics

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Research article

First published 2015-5

Fast terminal sliding mode control based on extended state observer for swing nozzle of anti-aircraft missile

Lianghua Sun, Weihong Wang, Ran Yi [...]

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

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Research article

First published 2015-3

Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control

Xiaodong Liu, Yu Zhang, Wanwei Huang [...]

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

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Other

First published 1980-10

Findings from a Study of Tactical Symbology for Fighter Aircraft Displays

Carole Jean Kopala

Proceedings of the Human Factors and Ergonomics Society Annual Meeting

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Other

First published 1980-10

Simulated A-10 Combat Environment

Robert S. Kellog, Dirk C. Prather, Carl H. Castore

Proceedings of the Human Factors and Ergonomics Society Annual Meeting

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Research article

First published 2024-7

Physical Optics Radar Cross Section predictions for an anti-ship cruise missile

Panagiotis Touzopoulos, Konstantinos C Zikidis

The Journal of Defense Modeling and Simulation: Applications,Methodology,Technology

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Research article

First published 1985-7

Chad: From Civil Strife to Big Power Rivalry

Kola Olufemi

India Quarterly: A Journal of International Affairs

Search results

An algorithm for selecting optimal controls to determine the estimators of the coefficients of a mathematical model for the dynamics of a self-propelled anti-aircraft missile system

Fast terminal sliding mode control based on extended state observer for swing nozzle of anti-aircraft missile

Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control

Findings from a Study of Tactical Symbology for Fighter Aircraft Displays

Simulated A-10 Combat Environment

Physical Optics Radar Cross Section predictions for an anti-ship cruise missile

Chad: From Civil Strife to Big Power Rivalry