Design of Missile Autopilot with Aerodynamic Lift and Reaction Jets Based on Auto Disturbance Rejection Controller

Abstract:

First a new autopilot design model is presented for the interceptor missile with the blended aerodynamic lift and reaction jet. The reaction jet can improve the response speed, but the structure of control system becomes more complex. Therefore how to design control strategy properly is an urgent problem. Second, considering the discrete property of the lateral pulse jet thrusters and the continuous property of the aerodynamic fins, a kind of ADRC (active disturbance rejection control) autopilot system was designed for the aerodynamic lift/reaction jet missile. Finally, through a testing in the simulation of MATLAB, it is shown that, due to the sufficient utilization of the reaction jet, there is a significant improvement in the fast response and robust performance of the proposed controller. It is applicable to design the autopilot of aerodynamic lift and reaction jet blended missile.

• Periodical: Advanced Materials Research (Volumes 472-475)
• Pages: 1036-1039
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.472-475.1036
• Online since: February 2012
• Authors: Chong Yang, Ke Zhang, Mei Bai Lu
• Keywords: Aerodynamic Lift and Reaction Jet, Auto Disturbance Rejection Controller, Compound Control

References

[1] Jing qing Han: From PID to Active Disturbance Rejection Control. industrial electronics, VOL56, NO. 3,900-907 march 2009.

[2] Dan Wu, Xian Kui Wang, Tong Zhao, Wei long Lv: Autolanding of Unmanned Aerial Vehicles based on Active Disturbance Rejection Control. 2005 IEEE Conference on Control Applications Toronto, Canada, August 28-31, (2005)

DOI: 10.1109/cca.2005.1507183

[3] Mario Innocenti, Ajay Thukral: Simultaneous Reaction Jet And Aerodynamic Control of Missile Systems". AlAA-93-3739-CP.

DOI: 10.2514/6.1993-3739

[4] Shao Chuntao, Zhou Di: Nonlinear Autopilot Design for Endoatmospheric Interceptors with Dual Control Systems. Systems and Control in Aerospace and Astronautics, 2008.

DOI: 10.1109/isscaa.2008.4776277

[5] Christian Tournes, Yuri Shtesse, Ilya Shkolnikov: Autopilot for Missiles Steered by Aerodynamic Lift and Divert Thrusters using Nonlinear Dynamic Sliding Manifolds. AIAA 2005-6382.

DOI: 10.2514/6.2005-6382

[6] D. Brett Ridgely, David Drakey, Louis Triplett, Cory Geise: Dynamic Control Allocation of a Missile with Tails and Reaction Jets. AIAA 2007-6671.

DOI: 10.2514/6.2007-6671

[7] Zhong Liu, Bing gang Cao, Xiao geng Liang, Xiao hong Jia: A Composite Dynamic Inverse Controller Design for Agile Missile. 6th World Congress on Intelligent Control and Automation, June 21 - 23, 2006, Dalian.

DOI: 10.1109/wcica.2006.1712480

[8] Ajay Thukral and Mario Innocenti: A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, Vol: 6, No: 3.359-372.

DOI: 10.1109/87.668037

[9] Kevin A. Wise David J. Broy: Agile missile dynamics and control. AIAA-96-3912.

[10] Qi SHeng Sui, Xin Li, Yong Hua Fan: Design of Autopilot for Aerodynamic/ Reaction-jet Multiple Control Missile. 2008 International Conference on Intelligent Computation Technology and Automation, pp.337-342.

DOI: 10.1109/icicta.2008.101