Study on dynamic decoupling design by using INA method for cruise missile

Xu Jiangtao; Cui Naigang; Tian Jichao; Liu Hongliang

doi:10.1109/ISSCAA.2008.4776389

Study on dynamic decoupling design by using INA method for cruise missile

Xu Jiangtao^*
, Cui Naigang
, Tian Jichao
, Liu Hongliang

^*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 non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.

Original language	English
DOIs	https://doi.org/10.1109/ISSCAA.2008.4776389
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.2008.4776389

Cite this

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abstract = "The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.",

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year = "2008",

doi = "10.1109/ISSCAA.2008.4776389",

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AU - Naigang, Cui

AU - Jichao, Tian

AU - Hongliang, Liu

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N2 - The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.

AB - The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.

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Y2 - 10 December 2008 through 12 December 2008

ER -

Study on dynamic decoupling design by using INA method for cruise missile

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