Precision Post-Stall Landing Using NMPC With Learned Aerodynamics

被引:2
|
作者
Basescu, Max [1 ]
Yeh, Bryanna [1 ]
Scheuer, Luca [1 ]
Wolfe, Kevin [1 ]
Moore, Joseph [1 ]
机构
[1] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20723 USA
关键词
Atmospheric modeling; Aircraft; Aerodynamics; Loading; Vehicle dynamics; Real-time systems; Predictive control; Aerial systems; Mechanics and control; aerial systems; Perception and autonomy; field robots; OPTIMIZATION; MANEUVERS;
D O I
10.1109/LRA.2023.3264738
中图分类号
TP24 [机器人技术];
学科分类号
080202 ; 1405 ;
摘要
In this letter, we present an approach for achieving precision post-stall landings with medium-sized Group 1 Unmanned Aerial Systems (UAS). To do this, we employ an aggressive dive-and-stall maneuver to significantly reduce maneuver distance, time, and touchdown speed. Our approach relies on a nonlinear model predictive control (NMPC) algorithm and learned aerodynamic coefficients to achieve accuracy and reliability in the presence of wind disturbances. We demonstrate our approach in hardware with a 60-inch wingspan, 4.2 kg fixed-wing UAS, and show the ability to land with low speed and high accuracy using minimal throttle.
引用
收藏
页码:3031 / 3038
页数:8
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