Blended control system design for agile missile with lateral jets and aerodynamic surfaces

Yongtao Bi; Yu Yao; Kemao Ma

doi:10.1109/ISSCAA.2008.4776286

Blended control system design for agile missile with lateral jets and aerodynamic surfaces

Yongtao Bi^*
, Yu Yao
, Kemao Ma

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Contribution to conference › Paper › peer-review

4 Scopus citations

Abstract

The longitudinal dynamic uncertain model of agile missiles with blended lateral jets and aerodynamic surfaces is established. Then a kind of modularization design scheme is proposed: considering the uncertainties and jet interaction of the blended system, the controller is designed based on the structured singular value synthesis; considering the control constraints of aerodynamic surfaces and lateral jet thrusters, the control allocation is achieved by applying redistributed pseudo inverse (RPI) method. Finally, the simulation results show that the designed blended control system can track the overload command rapidly and accurately, and it has robust performance for model uncertainty and jet interaction, moreover, control allocation between aerodynamic surfaces and lateral thrusters is appropriate, which can avoid the aerodynamic surface deflection saturation.

Original language	English
DOIs	https://doi.org/10.1109/ISSCAA.2008.4776286
State	Published - 2008
Event	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 - Shenzhen, China Duration: 10 Dec 2008 → 12 Dec 2008

Conference

Conference	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008
Country/Territory	China
City	Shenzhen
Period	10/12/08 → 12/12/08

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10.1109/ISSCAA.2008.4776286

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title = "Blended control system design for agile missile with lateral jets and aerodynamic surfaces",

abstract = "The longitudinal dynamic uncertain model of agile missiles with blended lateral jets and aerodynamic surfaces is established. Then a kind of modularization design scheme is proposed: considering the uncertainties and jet interaction of the blended system, the controller is designed based on the structured singular value synthesis; considering the control constraints of aerodynamic surfaces and lateral jet thrusters, the control allocation is achieved by applying redistributed pseudo inverse (RPI) method. Finally, the simulation results show that the designed blended control system can track the overload command rapidly and accurately, and it has robust performance for model uncertainty and jet interaction, moreover, control allocation between aerodynamic surfaces and lateral thrusters is appropriate, which can avoid the aerodynamic surface deflection saturation.",

author = "Yongtao Bi and Yu Yao and Kemao Ma",

year = "2008",

doi = "10.1109/ISSCAA.2008.4776286",

language = "英语",

note = "2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 ; Conference date: 10-12-2008 Through 12-12-2008",

}

TY - CONF

T1 - Blended control system design for agile missile with lateral jets and aerodynamic surfaces

AU - Bi, Yongtao

AU - Yao, Yu

AU - Ma, Kemao

PY - 2008

Y1 - 2008

N2 - The longitudinal dynamic uncertain model of agile missiles with blended lateral jets and aerodynamic surfaces is established. Then a kind of modularization design scheme is proposed: considering the uncertainties and jet interaction of the blended system, the controller is designed based on the structured singular value synthesis; considering the control constraints of aerodynamic surfaces and lateral jet thrusters, the control allocation is achieved by applying redistributed pseudo inverse (RPI) method. Finally, the simulation results show that the designed blended control system can track the overload command rapidly and accurately, and it has robust performance for model uncertainty and jet interaction, moreover, control allocation between aerodynamic surfaces and lateral thrusters is appropriate, which can avoid the aerodynamic surface deflection saturation.

AB - The longitudinal dynamic uncertain model of agile missiles with blended lateral jets and aerodynamic surfaces is established. Then a kind of modularization design scheme is proposed: considering the uncertainties and jet interaction of the blended system, the controller is designed based on the structured singular value synthesis; considering the control constraints of aerodynamic surfaces and lateral jet thrusters, the control allocation is achieved by applying redistributed pseudo inverse (RPI) method. Finally, the simulation results show that the designed blended control system can track the overload command rapidly and accurately, and it has robust performance for model uncertainty and jet interaction, moreover, control allocation between aerodynamic surfaces and lateral thrusters is appropriate, which can avoid the aerodynamic surface deflection saturation.

UR - https://www.scopus.com/pages/publications/66449137523

U2 - 10.1109/ISSCAA.2008.4776286

DO - 10.1109/ISSCAA.2008.4776286

M3 - 论文

AN - SCOPUS:66449137523

T2 - 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008

Y2 - 10 December 2008 through 12 December 2008

ER -

Blended control system design for agile missile with lateral jets and aerodynamic surfaces

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