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Published in 2017 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2016.12.013
Abstract: Abstract A robust entry guidance law based on terminal sliding mode and second-order differentiator is designed for trajectory tracking in this paper. The bank angle is regarded as the control variable. A novel nonlinear compound…
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Keywords:
nonlinear compound;
entry guidance;
controller;
trajectory tracking ... See more keywords
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Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2018.06.031
Abstract: Abstract This paper aims at developing an autonomous entry guidance method that requires no mission-dependent adjustments and will be applicable to a wide range of entry scenarios with worldwide destinations. Firstly, a nonlinear reduced-order entry…
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Keywords:
autonomous entry;
entry guidance;
method;
guidance ... See more keywords
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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.106361
Abstract: Abstract With the control constraints taken into account, the Mars entry guidance problem of the entry vehicle with a mid-lift-to-drag ratio is investigated in this paper. A dual-loop guidance framework is proposed that the bank…
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Keywords:
bank angle;
entry guidance;
guidance;
mars entry ... See more keywords
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Published in 2018 at "Transactions of the Institute of Measurement and Control"
DOI: 10.1177/0142331217735050
Abstract: Re-entry guidance is one of the primary tasks of a global strike mission. Hypersonic and common aero vehicles are currently being investigated for missions like this. This paper proposes a guidance law considering not only…
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Keywords:
hypersonic vehicle;
fly;
entry guidance;
guidance ... See more keywords