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Finite-time stabilization-based trajectory tracking under disturbances for entry vehicles

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

For the entry guidance based on a nominal trajectory, trajectory tracking is an important part, by which the nominal trajectory is followed and several constraints can be observed. In order to reject disturbance and achieve good tracking performance in trajectory tracking, a finite-time trajectory tracking method is presented. Utilizing the differential flatness theory, a linear tracking error system can be derived from the nonlinear point-mass dynamics of an entry vehicle. A disturbance compensator is designed based on linear extended state observers. The compensator observes the disturbances in the tracking error system, and then compensates the disturbances in the following tracking law. To track the nominal trajectory, a finite-time tracking law with disturbance compensation is derived using a linear finite-time stabilization method. This method ensures that the tracking error is finite-time stable and the settling time of the tracking error is within a specified range. Numerical simulation demonstrates the proposed trajectory tracking law. Under various disturbances, good tracking performance is achieved and all constraints are observed. The proposed trajectory tracking method is effective.

Original languageEnglish
Title of host publication2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1943-1948
Number of pages6
ISBN (Electronic)9781479946990
DOIs
StatePublished - 12 Jan 2015
Event6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, China
Duration: 8 Aug 201410 Aug 2014

Publication series

Name2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Conference

Conference6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Country/TerritoryChina
CityYantai
Period8/08/1410/08/14

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