@inproceedings{32d3029f69804b799555b9f973649e26,
title = "A novel unified modeling method and adaptive sliding mode control based on differential inclusion for hypersonic re-entry vehicle",
abstract = "A novel unified modeling approach is proposed to model the multi-model control system for hypersonic re-entry vehicle in wide flight envelope based on differential inclusion. Then based on the unified control model, an adaptive estimator is deigned to estimate the uncertain and un-modeled dynamics parameters. The real-time compensation for the systematic parameters with weight based on coefficient of variation is implemented to prevent the aged model. Afterwards, a modified adaptive nonsingular terminal sliding mode controller by introducing integral sliding mode surface is devised to realize the high precise robust control for hypersonic re-entry vehicle based on the unified control model with parameter dynamic match. Finally, the numerical simulation results verify the efficiency of the modeling approach and controller.",
author = "Jianjun Luo and Caisheng Wei and Baichun Gong and Jianping Yuan",
year = "2016",
language = "英语",
isbn = "9780877036296",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "1799--1810",
editor = "Turner, {James D.} and Wawrzyniak, {Geoff G.} and Cerven, {William Todd} and Manoranjan Majji",
booktitle = "Astrodynamics 2015",
note = "AAS/AIAA Astrodynamics Specialist Conference, ASC 2015 ; Conference date: 09-08-2015 Through 13-08-2015",
}