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Journal Articles

A Deployment Approach Toward Time-Energy Efficient Robust Performance for Interceptors

Arunava Banerjee, Abdelaziz Salah Saidi, Abdullah A. Algethami, Mashuq un Nabi

J. Dyn. Sys., Meas., Control. October 2022, 144(10): 101002.

Paper No: DS-21-1020

DOI: https://doi.org/10.1115/1.4055022

Published Online: August 3, 2022

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Topics: Algorithms, Control equipment, Design, Dynamics (Mechanics), Errors, Missiles, Robust control, Stability, Uncertainty, Sliding mode control

Journal Articles

Constrained Quasi-Spectral MPSP With Application to High-Precision Missile Guidance With Path Constraints

Sabyasachi Mondal, Radhakant Padhi

J. Dyn. Sys., Meas., Control. March 2021, 143(3): 031001.

Paper No: DS-19-1461

DOI: https://doi.org/10.1115/1.4048488

Published Online: October 15, 2020

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Topics: Algorithms, Computer programming, Deflection, Dynamics (Mechanics), Flight, Missile guidance systems, Optimization, Simulation, Optimal control, Missiles

Journal Articles

Observer-Based Guidance Law With Impact Angle Constraint

Pingping Qu, Di Zhou, Sheng Sun

J. Dyn. Sys., Meas., Control. November 2017, 139(11): 114504.

Paper No: DS-16-1280

DOI: https://doi.org/10.1115/1.4036664

Published Online: July 10, 2017

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Topics: Autopilots, Design, Dynamics (Mechanics), Missiles, Simulation results, Accounting

Journal Articles

Adaptive Self-Learning Fuzzy Autopilot Design for Uncertain Bank-to-Turn Missiles

Hai-Jun Rong, Zhao-Xu Yang, Pak Kin Wong, Chi Man Vong

J. Dyn. Sys., Meas., Control. April 2017, 139(4): 041002.

Paper No: DS-15-1419

DOI: https://doi.org/10.1115/1.4035091

Published Online: February 6, 2017

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Topics: Autopilots, Design, Errors, Missiles, Stability, Uncertainty, Algorithms, Dynamics (Mechanics), Fuzzy logic

Journal Articles

Adaptive Augmenting Control Design for Time-Varying Polytopic Systems

Hessam Mahdianfar, Emmanuel Prempain

J. Dyn. Sys., Meas., Control. January 2017, 139(1): 011005.

Paper No: DS-15-1440

DOI: https://doi.org/10.1115/1.4034420

Published Online: September 22, 2016

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Topics: Control equipment, Design, Missiles, Stability, Errors, Autopilots, Closed loop systems, Uncertainty, State feedback

Journal Articles

Three-Dimensional Impact Angle Guidance Laws Based on Model Predictive Control and Sliding Mode Disturbance Observer

Shaoming He, Wei Wang, Jiang Wang

J. Dyn. Sys., Meas., Control. August 2016, 138(8): 081006.

Paper No: DS-15-1318

DOI: https://doi.org/10.1115/1.4033272

Published Online: May 25, 2016

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Topics: Composite materials, Design, Errors, Simulation results, Missiles, Stability, Predictive control, Simulation

Journal Articles

Robust Control of Uncertain Nonlinear Systems: A Nonlinear DOBC Approach

Wen-Hua Chen, Jun Yang, Zhenhua Zhao

J. Dyn. Sys., Meas., Control. July 2016, 138(7): 071002.

Paper No: DS-14-1436

DOI: https://doi.org/10.1115/1.4033018

Published Online: May 3, 2016

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Topics: Control equipment, Nonlinear systems, Robust control, Robustness, Springs, Uncertainty, Scalars, Stability, Closed loop systems, Design

Journal Articles

Finite Time Convergence Guidance Law Accounting for Missile Autopilot

Pingping Qu, Chuntao Shao, Di Zhou

J. Dyn. Sys., Meas., Control. May 2015, 137(5): 051014.

Paper No: DS-13-1232

DOI: https://doi.org/10.1115/1.4029241

Published Online: May 1, 2015

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Topics: Accounting, Autopilots, Missiles, Simulation results, Design, Sliding mode control

Journal Articles

A Discrete Sliding-Mode Guidance Law

Di Zhou, Sheng Sun, Jing Yang Zhou, Kok Lay Teo

J. Dyn. Sys., Meas., Control. February 2015, 137(2): 024501.

Paper No: DS-14-1062

DOI: https://doi.org/10.1115/1.4028038

Published Online: September 10, 2014

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Topics: Design, Missiles, Simulation results, Missile guidance systems

Journal Articles

A Guidance Law With Terminal Impact Angle Constraint Accounting for Missile Autopilot

Di Zhou, Pingping Qu, Sheng Sun

J. Dyn. Sys., Meas., Control. September 2013, 135(5): 051009.

Paper No: DS-12-1144

DOI: https://doi.org/10.1115/1.4024202

Published Online: June 6, 2013

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Topics: Autopilots, Design, Missiles, Accounting, Dynamics (Mechanics), Flight

Journal Articles

Partial Stabilization Approach to 3-Dimensional Guidance Law Design

T. Binazadeh, M. J. Yazdanpanah

J. Dyn. Sys., Meas., Control. November 2011, 133(6): 064504.

DOI: https://doi.org/10.1115/1.4004575

Published Online: November 22, 2011

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Topics: Design, Missiles, Stability, Missile guidance systems, Simulation

Journal Articles

Nonlinear Control for Missile Terminal Guidance

Der-Cherng Liaw, Yew-Wen Liang, Chiz-Chung Cheng

J. Dyn. Sys., Meas., Control. December 2000, 122(4): 663–668.

DOI: https://doi.org/10.1115/1.1316796

Published Online: February 4, 2000

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Topics: Design, Missiles, Navigation, Missile guidance systems

Journal Articles

A Short-Range Air Combat Study

Bernt Ja¨rmark

J. Dyn. Sys., Meas., Control. December 1989, 111(4): 619–622.

DOI: https://doi.org/10.1115/1.3153103

Published Online: December 1, 1989

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Topics: Algorithms, Dynamic programming, Missiles, Numerical analysis, Warfare

Journal Articles

Impact Force Prediction Using Measured Frequency Response Functions

R. J. Thornhill, C. C. Smith

J. Dyn. Sys., Meas., Control. December 1983, 105(4): 227–231.

DOI: https://doi.org/10.1115/1.3140663

Published Online: December 1, 1983

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Topics: Frequency response, Aluminum castings, Fourier transforms, Hardware, Missiles, Steel

Journal citation

NARROW

A Deployment Approach Toward Time-Energy Efficient Robust Performance for Interceptors

Constrained Quasi-Spectral MPSP With Application to High-Precision Missile Guidance With Path Constraints

Observer-Based Guidance Law With Impact Angle Constraint

Adaptive Self-Learning Fuzzy Autopilot Design for Uncertain Bank-to-Turn Missiles

Adaptive Augmenting Control Design for Time-Varying Polytopic Systems

Three-Dimensional Impact Angle Guidance Laws Based on Model Predictive Control and Sliding Mode Disturbance Observer

Robust Control of Uncertain Nonlinear Systems: A Nonlinear DOBC Approach

Finite Time Convergence Guidance Law Accounting for Missile Autopilot

A Discrete Sliding-Mode Guidance Law

A Guidance Law With Terminal Impact Angle Constraint Accounting for Missile Autopilot

Partial Stabilization Approach to 3-Dimensional Guidance Law Design

Nonlinear Control for Missile Terminal Guidance

A Short-Range Air Combat Study

Impact Force Prediction Using Measured Frequency Response Functions

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