NDLI: Approach and landing guidance based on sliding mode control and input-to-state stability

Content Provider	IEEE Xplore Digital Library
Author	Yan Han Tan Shuping
Copyright Year	2015
Description	Author affiliation: Sci. & Technol. on Space Intell. Control Lab., Beijing Inst. of Control Eng., Beijing, China (Yan Han; Tan Shuping)
Abstract	This paper presents a new guidance law based on sliding-mode control and input-to-state stability (ISS) for approach and landing of a reusable launch vehicle (RLV). According to the idea of reference-trajectory guidance, the sliding mode surface is chosen to be a linear combination of the reference-trajectory tracking error and its rate, and a guidance law is designed to make the dynamics of the sliding mode surface be ISS with respect to bounded uncertainties. Then, by introducing class KL-like function, it is proved that the influence of uncertainties on reference-trajectory tracking error can be close to zero by adjusting the guidance parameters. The numerical simulation confirms the effectiveness of the proposed design approach.
Starting Page	5397
Ending Page	5401
File Size	3784592
Page Count	5
File Format	PDF
ISBN	9789881563897
ISSN	19341768
DOI	10.1109/ChiCC.2015.7260483
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2015-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Technical Committee on Control Theory, Chinese Association of Automation
Subject Keyword	Uncertainty Reference trajectory Input-to-state stability Stability analysis Robustness Trajectory Sliding mode control Numerical stability Reusable launch vehicles Guidance law Vehicles Approach and landing phase
Content Type	Text
Resource Type	Article

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