Reusable Launch Vehicle Control in Multiple-Time-Scale Sliding Modes
نویسندگان
چکیده
منابع مشابه
Robust Integral Sliding-Mode Control of an Aerospace Launch Vehicle
An analysis of on-line autonomous robust tracking controller based on variable structure control is presented for an aerospace launch vehicle. Decentralized sliding-mode controller is designed to achieve the decoupled asymptotic tracking of guidance commands upon plant uncertainties and external disturbances. Development and application of the controller for an aerospace launch vehicle during a...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2000
ISSN: 0731-5090,1533-3884
DOI: 10.2514/2.4669