Compound Control Methodology for a Robust Missile Autopilot Design-Reference-Cited by-同舟云学术

Compound Control Methodology for a Robust Missile Autopilot Design

Published:2015-11 Issue:6 Volume:28 Page:04014145
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

He Shaoming¹,Lin Defu²,Wang Jiang³

Affiliation:

1. Postgraduate Student, School of Aerospace Engineering, Beijing Institute of Technology, Haidian District, Beijing 100081, P.R. China (corresponding author).

2. Professor, School of Aerospace Engineering, Beijing Institute of Technology, Haidian District, Beijing 100081, P.R. China.

3. Lecturer, School of Aerospace Engineering, Beijing Institute of Technology, Haidian District, Beijing 100081, P.R. China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000484

Reference33 articles.

1. Continuous finite-time stabilization of the translational and rotational double integrators

2. Proportional Guidance and CDM Control Synthesis for a Short-Range Homing Surface-to-Air Missile

3. Nonlinear Disturbance Observer-Enhanced Dynamic Inversion Control of Missiles

4. Fan J. F. and Su Z. (2010). “Missile longitudinal autopilot design using backstepping approach.” Proc. IEEE Aerospace Conf. New York.

5. Performance Analysis of Generalized Extended State Observer in Tackling Sinusoidal Disturbances

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