Altitude Measurement-Based Optimization of the Landing Process of UAVs

被引:3
|
作者
Horla, Dariusz [1 ]
Giernacki, Wojciech [1 ]
Cieslak, Jacek [1 ,2 ]
Campoy, Pascual [3 ]
机构
[1] Poznan Univ Tech, Fac Automat Control Robot & Elect Engn, Inst Robot & Machine Intelligence, Ul Piotrowo 3a, PL-60965 Poznan, Poland
[2] ITTI Sp Zoo, Ul Rubiez 46, PL-62612 Poznan, Poland
[3] Univ Politecn Madrid UPM, Comp Vis & Aerial Robot Grp CVAR, Ctr Automat & Robot CAR, Madrid 28006, Spain
关键词
optimization; energy; UAV; landing;
D O I
10.3390/s21041151
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
The paper addresses the loop shaping problem in the altitude control of an unmanned aerial vehicle to land the flying robot with a specific landing scenario adopted. The proposed solution is optimal, in the sense of the selected performance indices, namely minimum-time, minimum-energy, and velocity-penalized related functions, achieving their minimal values, with numerous experiments conducted throughout the development and preparation to the Mohamed Bin Zayed International Robotics Challenge (MBZIRC 2020). A novel approach to generation of a reference altitude trajectory is presented, which is then tracked in a standard, though optimized, control loop. Three landing scenarios are considered, namely: minimum-time, minimum-energy, and velocity-penalized landing scenarios. The experimental results obtained with the use of the Simulink Support Package for Parrot Minidrones, and the OptiTrack motion capture system proved the effectiveness of the proposed approach.
引用
收藏
页码:1 / 26
页数:26
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