Supersonic Missile Control with PI Sliding Mode Method

Qiang Ma; Yu Qiang Jin

doi:10.4028/www.scientific.net/AMR.295-297.1773

Paper Titles

Management of Bio-Engineering Equipment - Take Ventilation and Mechanical Agitation Fermenter for Example
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Overload Control of Supersonic Missile System
p.1761

Modeling and Dynamic Simulation of Tracked Vehicle in Vortex
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A Steering Wheel System and Controller for the Driving Simulator
p.1768

Supersonic Missile Control with PI Sliding Mode Method
p.1773

Analysis of Characteristics of Potential Mud-Rock Flow in Huyu Valley
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Consider the Effect of the Variation of Underground Water Level to the Superstructure with the Pile Foundation in Different Burying Depth
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Construction of Customer Knowledge Management Platform Based on TRIZ
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Micro-Hole Machined by Electrochemical Discharge Machining (ECDM) with High Speed Rotating Cathode
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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 295-297Supersonic Missile Control with PI Sliding Mode...

Supersonic Missile Control with PI Sliding Mode Method

Abstract:

Comparing with traditional adaptive methods, a very simple PI sliding mode controller is designed for uncertain nonlinear missile systems with the help of two main assumptions which are also testified to be reasonable.The construction of PI control for sliding surface is novel and effective. Also, the proof of PI type control law is unique in this paper.

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Periodical:

Advanced Materials Research (Volumes 295-297)

Pages:

1773-1776

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.295-297.1773

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Online since:

July 2011

Authors:

Qiang Ma, Yu Qiang Jin

Keywords:

Control, Missile, Nonlinear, Sliding Mode, Uncertainty

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References

[1] Seung-Hwan Kim, Yoon-Sik Kim, Chanho Song, Control engineering practice, 12(2004) pp.149-154

Google Scholar

[2] Hull, R.A., & Z. Qu, 1995. Design and evaluation of robust nonlinear missile autopilot from a performance perspective. Proceedings of the ACC, 189–193

Google Scholar

[3] Junwei Lei, Xinyu Wang, Yinhua Lei, , Physics Letters A, Volume 373, Issue 14, 23 March 2009, Pages 1249-1256

Google Scholar

[4] Junwei Lei, Xinyu Wang, Yinhua Lei, , Communications in Nonlinear Science and Numerical Simulation, Volume 14, Issue 8, August 2009, Pages 3439-3448

Google Scholar

[5] Xinyu Wang, Junwei Lei, Changpeng Pan, Applied Mathematics and Computation, 185 (2007) pp.989-1002

Google Scholar