Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique

Author:

Mehrabian Ali Reza1,Roshanian Jafar2

Affiliation:

1. Control and Intelligent Processing Center of Excellence, Department of Mechanical Engineering, University of Tehran, Tehran, Iran

2. Department of Aerospace Engineering, K N Toosi University of Technology, Tehran, Iran

Abstract

This paper presents an application of adaptive control techniques to the design of skid-to-turn missile autopilot. The involved simplified adaptive controller is developed by combining gain scheduling approach with the eigenstructure assignment control design. A linear interpolation method is proposed to generate linear parameter-varying controller from a finite set of linear time-invariant controllers. Results of simulations are reported to demonstrate the performance, stability, and robustness of the considered autopilot.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 19 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Robust Missile Autopilot Design Using Two Time-Scale Separation;IEEE Transactions on Aerospace and Electronic Systems;2018-06

2. Multi-Mode Electric Actuator Dynamic Modelling for Missile Fin Control;Aerospace;2017-06-14

3. Pitch and flight path controller design for F-16 aircraft using combination of LQR and EA techniques;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-04-10

4. Generalized ESO and Predictive Control Based Robust Autopilot Design;Journal of Control Science and Engineering;2016

5. Compound Control Methodology for a Robust Missile Autopilot Design;Journal of Aerospace Engineering;2015-11

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