有限时间收敛的阻力加速度跟踪进入制导律

PDF (PC)

Like

Knowledge

DragTracking Guidance for Entry Vehicles with Finite Time

DragTracking Guidance for Entry Vehicles with Finite Time

Abstract

References

Metrics

Abstract

Cite this article

share this article

References

Related Articles 14

Metrics

Comments

Recommended 0

doi:10.3969/j.issn.1674-1579.2018.01.005

›› 2018, Vol. 44 ›› Issue (1): 38-44.doi: 10.3969/j.issn.1674-1579.2018.01.005

Previous Articles Next Articles

YAN Han, HE Ying-Zi

1.Beijing Institute of Control Engineering, Beijing 100190, China;2.Science and Technology on Space Intelligent Control Laboratory, Beijing 100190, China.

Online:2018-02-26 Published:2018-03-15
Supported by:
Supported by State key Program of National Science of China (61403030).

Abstract: Abstract：A robust entry guidance law with finite time convergence is designed for dragtracking in this paper. The bank angle is regarded as the control variable. First, a robust sliding mode control (SMC) method, which can guarantee the finite time convergence, is proposed for a class of nonlinear systems with uncertainties and disturbances. Then, after the drag dynamics is given, the finite time guidance law is designed based on the proposed SMC method. A 1 000run Monte Carlo simulation shows the effectiveness of the presented approach.

Key words: Keywords：entry vehicle, dragtracking, sliding mode control, finite time convergence, Monte Carlo simulation

CLC Number:

V448.2

YAN Han, HE Ying-Zi. DragTracking Guidance for Entry Vehicles with Finite Time[J]., 2018, 44(1): 38-44.

0
/ Save 0 / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2018.01.005

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2018/V44/I1/38

Viewed

Full text

From	Others	local

Times	2	61
Rate	3%	97%

Abstract

Just accepted	Online first	Issue

0	0	75

	From	Others

	Times	75
	Rate	100%

Cited

Web of Science	Crossref	ScienceDirect	Search for Citations in Google Scholar >>


This page requires you have already subscribed to WoS.

Shared

[1]	ZHANG Wenhui, CHEN Haowen, WEN Zhi, YE Xiaoping. Sliding Mode Control of Flexible Joint Space Robot for Unknown Target [J]. Aerospace Contrd and Application, 2021, 47(3): 49-56.
[2]	DENG Ruchuan, ZHAO Di, ZHANG Shan, GOU Hao, FU Jianhao, ZHENG Liang, FEI Ling. Performance Analysis of the Combined Speed Sliding Mode and Current Prediction Controller of Permanent Magnet Synchronous Motor [J]. Aerospace Contrd and Application, 2021, 47(3): 64-72.
[3]	HE Jingjiu, YUAN Changqing, ZUO Chenyi. Formation Keeping Control of Hybrid Propulsion ThreeSatellite Coulomb Formation in Geostationary Orbit [J]. Aerospace Contrd and Application, 2021, 47(1): 15-21.
[4]	LU Ming, LIANG Zhulin, XU Zhangfan. Dynamic Modeling and Control of Flexible Support Control Moment Gyroscope [J]. Aerospace Contrd and Application, 2021, 47(1): 40-46.
[5]	XUE Chao, TAN Shu-Ping, LIU He-Long. Librational Controller Design for a Tethered Satellite System during Orbital Maneuvering [J]. , 2017, 43(2): 21-27.
[6]	GENG Jie, 吕Nan , WANG Tao, GONG Jing-Gang. A Novel FiniteTime Sliding Mode Attitude Controller for Spacecraft [J]. , 2016, 42(4): 30-.
[7]	XU Wei, WU Hai-Lei, LU Shan, LIU Fu-Cheng. A High Precision Attitude Tracking Control Method for Highly Eccentric Orbit Spacecraft Rendezvous with a HEO Target [J]. , 2015, 41(2): 6-11.
[8]	GUO Chaoli, ZHANG Duzhou, WANG Shuyi. Sliding Mode Control for Rate Damping of Underactuated Spacecraft [J]. , 2013, 39(4): 12-17.
[9]	ZHONG Chen-Xing, GUO Yu, ZHOU Chuan, CHEN Qing-Wei. On Sliding Mode Variable Structure Control and Chattering Reduction for Flexible Spacecraft [J]. , 2013, 39(2): 24-29.
[10]	XING Jian, QI Rui-Yun. Adaptive Sliding-Mode Attitude Control of Spacecraft with Fuel Sloshing [J]. , 2013, 39(2): 42-47.
[11]	HU Shao-Chun, SUN Cheng-Qi, LIU Yi-Wu. On Midcourse Correction of Transfer Trajectory for Halo Orbiters [J]. , 2012, 38(5): 21-27.
[12]	HU Min, ZENG Guo-Qiang. FiniteTime Control for Satellite Formation Flight [J]. , 2012, 38(1): 23-28.
[13]	LI Huifeng，SUN Wenchong. Index Approach Law Based Sliding Control for A Hypersonic Vehicle LI Huifeng，SUN Wenchong [J]. , 2009, 35(4): 39-43.
[14]	LIU Zhiyong1,2, HE Yingzi1,2. Integral Sliding Mode Control with Adaptive Parameters for Flying around Slowly Rotating Target [J]. , 2009, 35(4): 22-26.

Just accepted

Online first

Just accepted

Online first