Deceleration control by the coning motion for CAV terminal guidance without velocity profile

Denggao Ji; Bin Wu; Changwan Min; Zhenxi Guo; Zhen Xiao; Fenghua He

doi:10.1109/ChiCC.2016.7554255

Deceleration control by the coning motion for CAV terminal guidance without velocity profile

Denggao Ji
, Bin Wu
, Changwan Min
, Zhenxi Guo
, Zhen Xiao
, Fenghua He

School of Astronautics

Science and Technology on Space Physics Laboratory

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

1 Scopus citations

Abstract

The deceleration control by the coning motion without the velocity profile is proposed for common aero vehicle (CAV) terminal guidance, which restricted by velocity and position requisition. First, one-order approximate model of velocity and long range is derived, which transform the guidance deceleration control to closed loop guidance interrelated by terminal velocity. Velocity precision is improved by aerodynamics analysis and optimal guidance parameter design. Then, according to the characteristic of the coning motion target velocity and position precision meet the specified requirements, by orthogonal allocating the trajectory acceleration and the velocity over load. The simulation results show that, the method can achieve the high accuracy, adapt to serious disturbance and deviation without programming velocity profile beforehand and complex calculations.

Original language	English
Title of host publication	Proceedings of the 35th Chinese Control Conference, CCC 2016
Editors	Jie Chen, Qianchuan Zhao, Jie Chen
Publisher	IEEE Computer Society
Pages	5747-5751
Number of pages	5
ISBN (Electronic)	9789881563910
DOIs	https://doi.org/10.1109/ChiCC.2016.7554255
State	Published - 26 Aug 2016
Event	35th Chinese Control Conference, CCC 2016 - Chengdu, China Duration: 27 Jul 2016 → 29 Jul 2016

Publication series

Name	Chinese Control Conference, CCC
Volume	2016-August
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	35th Chinese Control Conference, CCC 2016
Country/Territory	China
City	Chengdu
Period	27/07/16 → 29/07/16

Keywords

A Coning Motion based Deceleration Control
Orthogonal Allocation
Reentry Vehicle
Vehicle General Design

Access to Document

10.1109/ChiCC.2016.7554255

Cite this

Ji, D., Wu, B., Min, C., Guo, Z., Xiao, Z., & He, F. (2016). Deceleration control by the coning motion for CAV terminal guidance without velocity profile. In J. Chen, Q. Zhao, & J. Chen (Eds.), Proceedings of the 35th Chinese Control Conference, CCC 2016 (pp. 5747-5751). Article 7554255 (Chinese Control Conference, CCC; Vol. 2016-August). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2016.7554255

@inproceedings{da2aac31e75f4adabf741d5b4b59d9e3,

title = "Deceleration control by the coning motion for CAV terminal guidance without velocity profile",

abstract = "The deceleration control by the coning motion without the velocity profile is proposed for common aero vehicle (CAV) terminal guidance, which restricted by velocity and position requisition. First, one-order approximate model of velocity and long range is derived, which transform the guidance deceleration control to closed loop guidance interrelated by terminal velocity. Velocity precision is improved by aerodynamics analysis and optimal guidance parameter design. Then, according to the characteristic of the coning motion target velocity and position precision meet the specified requirements, by orthogonal allocating the trajectory acceleration and the velocity over load. The simulation results show that, the method can achieve the high accuracy, adapt to serious disturbance and deviation without programming velocity profile beforehand and complex calculations.",

keywords = "A Coning Motion based Deceleration Control, Orthogonal Allocation, Reentry Vehicle, Vehicle General Design",

author = "Denggao Ji and Bin Wu and Changwan Min and Zhenxi Guo and Zhen Xiao and Fenghua He",

note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",

year = "2016",

month = aug,

day = "26",

doi = "10.1109/ChiCC.2016.7554255",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

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editor = "Jie Chen and Qianchuan Zhao and Jie Chen",

booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",

address = "美国",

}

Ji, D, Wu, B, Min, C, Guo, Z, Xiao, Z & He, F 2016, Deceleration control by the coning motion for CAV terminal guidance without velocity profile. in J Chen, Q Zhao & J Chen (eds), Proceedings of the 35th Chinese Control Conference, CCC 2016., 7554255, Chinese Control Conference, CCC, vol. 2016-August, IEEE Computer Society, pp. 5747-5751, 35th Chinese Control Conference, CCC 2016, Chengdu, China, 27/07/16. https://doi.org/10.1109/ChiCC.2016.7554255

Deceleration control by the coning motion for CAV terminal guidance without velocity profile. / Ji, Denggao; Wu, Bin; Min, Changwan et al.
Proceedings of the 35th Chinese Control Conference, CCC 2016. ed. / Jie Chen; Qianchuan Zhao; Jie Chen. IEEE Computer Society, 2016. p. 5747-5751 7554255 (Chinese Control Conference, CCC; Vol. 2016-August).

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

TY - GEN

T1 - Deceleration control by the coning motion for CAV terminal guidance without velocity profile

AU - Ji, Denggao

AU - Wu, Bin

AU - Min, Changwan

AU - Guo, Zhenxi

AU - Xiao, Zhen

AU - He, Fenghua

PY - 2016/8/26

Y1 - 2016/8/26

N2 - The deceleration control by the coning motion without the velocity profile is proposed for common aero vehicle (CAV) terminal guidance, which restricted by velocity and position requisition. First, one-order approximate model of velocity and long range is derived, which transform the guidance deceleration control to closed loop guidance interrelated by terminal velocity. Velocity precision is improved by aerodynamics analysis and optimal guidance parameter design. Then, according to the characteristic of the coning motion target velocity and position precision meet the specified requirements, by orthogonal allocating the trajectory acceleration and the velocity over load. The simulation results show that, the method can achieve the high accuracy, adapt to serious disturbance and deviation without programming velocity profile beforehand and complex calculations.

AB - The deceleration control by the coning motion without the velocity profile is proposed for common aero vehicle (CAV) terminal guidance, which restricted by velocity and position requisition. First, one-order approximate model of velocity and long range is derived, which transform the guidance deceleration control to closed loop guidance interrelated by terminal velocity. Velocity precision is improved by aerodynamics analysis and optimal guidance parameter design. Then, according to the characteristic of the coning motion target velocity and position precision meet the specified requirements, by orthogonal allocating the trajectory acceleration and the velocity over load. The simulation results show that, the method can achieve the high accuracy, adapt to serious disturbance and deviation without programming velocity profile beforehand and complex calculations.

KW - A Coning Motion based Deceleration Control

KW - Orthogonal Allocation

KW - Reentry Vehicle

KW - Vehicle General Design

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DO - 10.1109/ChiCC.2016.7554255

M3 - 会议稿件

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BT - Proceedings of the 35th Chinese Control Conference, CCC 2016

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PB - IEEE Computer Society

T2 - 35th Chinese Control Conference, CCC 2016

Y2 - 27 July 2016 through 29 July 2016

ER -

Deceleration control by the coning motion for CAV terminal guidance without velocity profile

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Keywords

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