Simulation of target image tracking when thrust and velocity change abruptly

Hai Lin; Xiaofang Wang

Simulation of target image tracking when thrust and velocity change abruptly

Hai Lin^*, Xiaofang Wang

^*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

Abstract

In terminal accelerating phase, abrupt changes of thrust and velocity of image guided missile will disturb image tracking and guidance loops in which the shooter is involved. A man-in-loop real-time simulation of tracking and guidance is taken to study this problem. The target, missile and image seeker in simulation system are expressed as mathematical models while the shooter and the controller are introduced into simulation system as hardware. Tracking error and guidance coefficient variety caused by abrupt thrust change is obtained and the stability of image tracking and trajectory is discussed.

Original language	English
Title of host publication	Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)
Editors	C. Zongij, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng, C. Zongji, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng
Pages	444-447
Number of pages	4
Publication status	Published - 2002
Event	Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai) - Shanghai, China Duration: 3 Nov 2002 → 6 Nov 2002

Publication series

Name	Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)

Conference

Conference	Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai)
Country/Territory	China
City	Shanghai
Period	3/11/02 → 6/11/02

Cite this

Lin, H., & Wang, X. (2002). Simulation of target image tracking when thrust and velocity change abruptly. In C. Zongij, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng, C. Zongji, F. Minrui, H. Guosen, P. Xiaoyuan, & X. Guangleng (Eds.), Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai) (pp. 444-447). (Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)).

Lin, Hai ; Wang, Xiaofang. / Simulation of target image tracking when thrust and velocity change abruptly. Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai). editor / C. Zongij ; F. Minrui ; H. Guosen ; P. Xiaoyuan ; X. Guangleng ; C. Zongji ; F. Minrui ; H. Guosen ; P. Xiaoyuan ; X. Guangleng. 2002. pp. 444-447 (Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)).

@inproceedings{1c4e1fe89019445da5da6ebc56f706fe,

title = "Simulation of target image tracking when thrust and velocity change abruptly",

abstract = "In terminal accelerating phase, abrupt changes of thrust and velocity of image guided missile will disturb image tracking and guidance loops in which the shooter is involved. A man-in-loop real-time simulation of tracking and guidance is taken to study this problem. The target, missile and image seeker in simulation system are expressed as mathematical models while the shooter and the controller are introduced into simulation system as hardware. Tracking error and guidance coefficient variety caused by abrupt thrust change is obtained and the stability of image tracking and trajectory is discussed.",

author = "Hai Lin and Xiaofang Wang",

year = "2002",

language = "English",

isbn = "7506255715",

series = "Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)",

pages = "444--447",

editor = "C. Zongij and F. Minrui and H. Guosen and P. Xiaoyuan and X. Guangleng and C. Zongji and F. Minrui and H. Guosen and P. Xiaoyuan and X. Guangleng",

booktitle = "Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)",

note = "Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai) ; Conference date: 03-11-2002 Through 06-11-2002",

}

Lin, H & Wang, X 2002, Simulation of target image tracking when thrust and velocity change abruptly. in C Zongij, F Minrui, H Guosen, P Xiaoyuan, X Guangleng, C Zongji, F Minrui, H Guosen, P Xiaoyuan & X Guangleng (eds), Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai). Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai), pp. 444-447, Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai), Shanghai, China, 3/11/02.

Simulation of target image tracking when thrust and velocity change abruptly. / Lin, Hai; Wang, Xiaofang.
Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai). ed. / C. Zongij; F. Minrui; H. Guosen; P. Xiaoyuan; X. Guangleng; C. Zongji; F. Minrui; H. Guosen; P. Xiaoyuan; X. Guangleng. 2002. p. 444-447 (Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)).

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

TY - GEN

T1 - Simulation of target image tracking when thrust and velocity change abruptly

AU - Lin, Hai

AU - Wang, Xiaofang

PY - 2002

Y1 - 2002

N2 - In terminal accelerating phase, abrupt changes of thrust and velocity of image guided missile will disturb image tracking and guidance loops in which the shooter is involved. A man-in-loop real-time simulation of tracking and guidance is taken to study this problem. The target, missile and image seeker in simulation system are expressed as mathematical models while the shooter and the controller are introduced into simulation system as hardware. Tracking error and guidance coefficient variety caused by abrupt thrust change is obtained and the stability of image tracking and trajectory is discussed.

AB - In terminal accelerating phase, abrupt changes of thrust and velocity of image guided missile will disturb image tracking and guidance loops in which the shooter is involved. A man-in-loop real-time simulation of tracking and guidance is taken to study this problem. The target, missile and image seeker in simulation system are expressed as mathematical models while the shooter and the controller are introduced into simulation system as hardware. Tracking error and guidance coefficient variety caused by abrupt thrust change is obtained and the stability of image tracking and trajectory is discussed.

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M3 - Conference contribution

AN - SCOPUS:0141543780

SN - 7506255715

T3 - Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)

SP - 444

EP - 447

BT - Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)

A2 - Zongij, C.

A2 - Minrui, F.

A2 - Guosen, H.

A2 - Xiaoyuan, P.

A2 - Guangleng, X.

A2 - Zongji, C.

A2 - Minrui, F.

A2 - Guosen, H.

A2 - Xiaoyuan, P.

A2 - Guangleng, X.

T2 - Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai)

Y2 - 3 November 2002 through 6 November 2002

ER -

Lin H, Wang X. Simulation of target image tracking when thrust and velocity change abruptly. In Zongij C, Minrui F, Guosen H, Xiaoyuan P, Guangleng X, Zongji C, Minrui F, Guosen H, Xiaoyuan P, Guangleng X, editors, Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai). 2002. p. 444-447. (Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)).

Simulation of target image tracking when thrust and velocity change abruptly

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