Minimum Jerk based Guidance for Autonomous Soft -Landing of Quadrotor

被引:0
|
作者
Kumar, P. S. V. S. Sai [1 ]
Padhi, Radhakant [2 ]
机构
[1] Indian Inst Sci Bangalore, Robert Bosch Ctr Cyber Phys Syst, Bangalore, Karnataka, India
[2] Indian Inst Sci Bangalore, Dept Aerosp Engn, Bangalore, Karnataka, India
来源
IFAC PAPERSONLINE | 2024年 / 57卷
关键词
Guidance navigation and control; Flying robots; Unmanned aerial vehicles; Autonomous soft-landing; Closed-form guidance; Optimal guidance; Time-to-go;
D O I
10.1016/j.ifacol.2024.05.019
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A novel soft-landing trajectory generation strategy for Unmanned Aerial Vehicles is presented in this paper. Towards this objective, a jerk minimization-based optimal control problem is formulated to generate the trajectory. Hard boundary constraints on position, velocity and acceleration are enforced to facilitate soft-landing and smooth handover between consecutive phases. An acceleration-based optimization problem is adopted to compute the time-to-go. The developed algorithm provides a closed-form solution, ensuring minimal computational requirements. Results obtained are illustrated through extensive simulations on a quadrotor platform. Simulation results show that this method produces smooth trajectories to soft land on the target even when the wind is introduced as a disturbance.
引用
收藏
页码:107 / 112
页数:6
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