Autopilot design for homing missiles considering guidance loop dynamics

Feng Tan; Mingzhe Hou; Haihong Zhao

doi:10.1109/ICICIP.2011.6008186

Autopilot design for homing missiles considering guidance loop dynamics

Feng Tan^*
, Mingzhe Hou
, Haihong Zhao

^*Corresponding author for this work

School of Astronautics

School of Mechatronics Engineering, Harbin Institute of Technology

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

1 Scopus citations

Abstract

The design problem for autopilot systems of homing missiles is investigated considering the guidance loop dynamics. The closed-loop guidance system is regarded as a reference model and the model reference tracking theory is employed to design the autopilot system. A parametric approach for the design of the feedforward tracking compensator and the global stabilizing feedback controller is given. According to the proposed method, the states of the guidance system are incorporated directly into the controller of the autopilot system and consequently the guidance loop dynamics can be well considered during the autopilot design procedure. Simulation results show the effect of the proposed method.

Original language	English
Title of host publication	Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011
Pages	1-5
Number of pages	5
Edition	PART 1
DOIs	https://doi.org/10.1109/ICICIP.2011.6008186
State	Published - 2011
Event	2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011 - Harbin, China Duration: 25 Jul 2011 → 28 Jul 2011

Publication series

Name	Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011
Number	PART 1

Conference

Conference	2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011
Country/Territory	China
City	Harbin
Period	25/07/11 → 28/07/11

Access to Document

10.1109/ICICIP.2011.6008186

Cite this

Tan, F., Hou, M., & Zhao, H. (2011). Autopilot design for homing missiles considering guidance loop dynamics. In Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011 (PART 1 ed., pp. 1-5). Article 6008186 (Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011; No. PART 1). https://doi.org/10.1109/ICICIP.2011.6008186

Tan, Feng ; Hou, Mingzhe ; Zhao, Haihong. / Autopilot design for homing missiles considering guidance loop dynamics. Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011. PART 1. ed. 2011. pp. 1-5 (Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011; PART 1).

@inproceedings{a4b82220448249969ec6c0cbe1960c11,

title = "Autopilot design for homing missiles considering guidance loop dynamics",

abstract = "The design problem for autopilot systems of homing missiles is investigated considering the guidance loop dynamics. The closed-loop guidance system is regarded as a reference model and the model reference tracking theory is employed to design the autopilot system. A parametric approach for the design of the feedforward tracking compensator and the global stabilizing feedback controller is given. According to the proposed method, the states of the guidance system are incorporated directly into the controller of the autopilot system and consequently the guidance loop dynamics can be well considered during the autopilot design procedure. Simulation results show the effect of the proposed method.",

author = "Feng Tan and Mingzhe Hou and Haihong Zhao",

year = "2011",

doi = "10.1109/ICICIP.2011.6008186",

language = "英语",

isbn = "9781457708145",

series = "Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011",

number = "PART 1",

pages = "1--5",

booktitle = "Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011",

edition = "PART 1",

note = "2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011 ; Conference date: 25-07-2011 Through 28-07-2011",

}

Tan, F , Hou, M & Zhao, H 2011, Autopilot design for homing missiles considering guidance loop dynamics. in Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011. PART 1 edn, 6008186, Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011, no. PART 1, pp. 1-5, 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011, Harbin, China, 25/07/11. https://doi.org/10.1109/ICICIP.2011.6008186

Autopilot design for homing missiles considering guidance loop dynamics. / Tan, Feng ; Hou, Mingzhe; Zhao, Haihong.
Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011. PART 1. ed. 2011. p. 1-5 6008186 (Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011; No. PART 1).

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

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AB - The design problem for autopilot systems of homing missiles is investigated considering the guidance loop dynamics. The closed-loop guidance system is regarded as a reference model and the model reference tracking theory is employed to design the autopilot system. A parametric approach for the design of the feedforward tracking compensator and the global stabilizing feedback controller is given. According to the proposed method, the states of the guidance system are incorporated directly into the controller of the autopilot system and consequently the guidance loop dynamics can be well considered during the autopilot design procedure. Simulation results show the effect of the proposed method.

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Tan F , Hou M, Zhao H. Autopilot design for homing missiles considering guidance loop dynamics. In Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011. PART 1 ed. 2011. p. 1-5. 6008186. (Proceedings of the 2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011; PART 1). doi: 10.1109/ICICIP.2011.6008186

Autopilot design for homing missiles considering guidance loop dynamics

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