Analysis for height control-loop of cruise missile to different kinds of autopilot

Qiuqiu Wen; Qunli Xia; Chuntao Cai

doi:10.1007/978-3-642-25646-2_66

Analysis for height control-loop of cruise missile to different kinds of autopilot

Qiuqiu Wen^*, Qunli Xia, Chuntao Cai

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Citation (Scopus)

Abstract

The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.

Original language	English
Title of host publication	Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011
Pages	507-514
Number of pages	8
DOIs	https://doi.org/10.1007/978-3-642-25646-2_66
Publication status	Published - 2011
Event	2011 International Conference on Automation and Robotics, ICAR 2011 - Dubai, United Arab Emirates Duration: 1 Dec 2011 → 2 Dec 2011

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	123 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	2011 International Conference on Automation and Robotics, ICAR 2011
Country/Territory	United Arab Emirates
City	Dubai
Period	1/12/11 → 2/12/11

Keywords

Height control
acceleration autopilot
attitude autopilot
gravity compensation

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10.1007/978-3-642-25646-2_66

Cite this

Wen, Q., Xia, Q., & Cai, C. (2011). Analysis for height control-loop of cruise missile to different kinds of autopilot. In Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011 (pp. 507-514). (Lecture Notes in Electrical Engineering; Vol. 123 LNEE). https://doi.org/10.1007/978-3-642-25646-2_66

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title = "Analysis for height control-loop of cruise missile to different kinds of autopilot",

abstract = "The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.",

keywords = "Height control, acceleration autopilot, attitude autopilot, gravity compensation",

author = "Qiuqiu Wen and Qunli Xia and Chuntao Cai",

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language = "English",

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booktitle = "Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011",

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Wen, Q , Xia, Q & Cai, C 2011, Analysis for height control-loop of cruise missile to different kinds of autopilot. in Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011. Lecture Notes in Electrical Engineering, vol. 123 LNEE, pp. 507-514, 2011 International Conference on Automation and Robotics, ICAR 2011, Dubai, United Arab Emirates, 1/12/11. https://doi.org/10.1007/978-3-642-25646-2_66

Analysis for height control-loop of cruise missile to different kinds of autopilot. / Wen, Qiuqiu ; Xia, Qunli; Cai, Chuntao.
Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011. 2011. p. 507-514 (Lecture Notes in Electrical Engineering; Vol. 123 LNEE).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.

AB - The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.

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Analysis for height control-loop of cruise missile to different kinds of autopilot

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Keywords

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