Towards adaptive autopilots for fixed-wing unmanned aerial vehicles

被引:0
|
作者
Baldi, Simone [1 ,2 ]
Roy, Spandan [3 ]
Yang, Kang [1 ]
机构
[1] Southeast Univ, Sch Cyber Sci & Engn, Nanjing, Peoples R China
[2] Southeast Univ, Sch Math, Nanjing, Peoples R China
[3] Int Inst Informat Technol Hyderabad IIIT H, Robot Res Ctr, Hyderabad, India
关键词
PATH-FOLLOWING CONTROL; SLIDING MODE; AIRCRAFT; UAV; NAVIGATION; ATTITUDE; SYSTEMS;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Control of fixed-wing Unmanned Aerial Vehicles (UAVs) is typically organized according to two layers: the low-level control or autopilot, and the high-level control or guidance. The disadvantage of this modular design is that an intelligent guidance layer may become ineffective if the autopilot layer cannot deal with uncertainty. In fact, the required knowledge derived from linearization of equations of motion (trimming points) makes most autopilots sensitive to uncertainty. In this work, we study an autopilot framework where the knowledge of the UAV dynamics and of trimming points is not required. The proposed design, tested with complex UAV dynamics, can emulate the behavior of a carefully tuned off-the-shelf autopilot, without using its a priori knowledge.
引用
收藏
页码:4724 / 4729
页数:6
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