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Aircraft flat-spin recovery using sliding-mode based attitude and altitude control
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-10-22 , DOI: 10.1177/0954410020964674 Salahudden 1 , Vijay S Dwivedi 1 , Prasiddha N Dwivedi 2 , Dipak K Giri 1 , Ajoy K Ghosh 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-10-22 , DOI: 10.1177/0954410020964674 Salahudden 1 , Vijay S Dwivedi 1 , Prasiddha N Dwivedi 2 , Dipak K Giri 1 , Ajoy K Ghosh 1
Affiliation
In the present paper, a control command to recover steady-straight-level flight from flat-oscillatory-stable-left-spin is developed using a sliding-mode based attitude and altitude control. Direct ...
中文翻译：
使用基于滑模的姿态和高度控制的飞机平旋恢复
在本文中，使用基于滑模的姿态和高度控制开发了从平振荡稳定左旋恢复稳定直线水平飞行的控制命令。直接的 ...
更新日期：2020-10-22
中文翻译：
使用基于滑模的姿态和高度控制的飞机平旋恢复
在本文中，使用基于滑模的姿态和高度控制开发了从平振荡稳定左旋恢复稳定直线水平飞行的控制命令。直接的 ...
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