Parametric method for spacecraft trajectory tracking control problem with stochastic thruster fault-Reference-Cited by-同舟云学术

Parametric method for spacecraft trajectory tracking control problem with stochastic thruster fault

Published:2016-10-20 Issue:17 Volume:10 Page:2331-2338
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Fu Yan‐Ming¹,Li Cheng‐Jing²

Affiliation:

1. Center for Control Theory and Guidance Technology, Harbin Institute of TechnologyP.O. Box 416Harbin150001People's Republic of China

2. Institute of Chemical Materials, CAEPP.O. Box 919‐314Mianyang621999People's Republic of China

Funder

National Natural Science Foundation of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2016.0353

Reference25 articles.

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3. Formation flying of multiple spacecraft with autonomous rendezvous and docking capability

4. Spacecraft intercept using minimum control energy and wait time;Leeghim H.;Celest. Mech. Dyn. Astr.,2013

5. A Decomposition-Based Approach to Linear Time-Periodic Distributed Control of Satellite Formations

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