Development of a fixed-wing vertical takeoff and landing aircraft as an autonomous vehicle

被引：0
|
作者：
Silva, Natassya B. F. [1 ]
Fontes, Joao V. C. [1 ]
Inoue, Roberto S. [2 ]
Branco, Kalinka R. L. J. C. [1 ]
机构：
[1] Univ Sao Paulo, Ave Trabalhador Sao Carlense 400, BR-13566590 Sao Carlos, SP, Brazil
[2] Univ Fed Sao Carlos UFS CAR, Rodovia Washington Lus,Km 235, BR-13565905 Sao Carlos, SP, Brazil
来源：
2017 LATIN AMERICAN ROBOTICS SYMPOSIUM (LARS) AND 2017 BRAZILIAN SYMPOSIUM ON ROBOTICS (SBR) | 2017年
基金：
巴西圣保罗研究基金会;
关键词：
FLIGHT;
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
Unmanned Aerial Vehicles (UAVs) with different configurations exist to supply requirements for diverse applications. One of them is the tailsitter that gathers complementary advantages from Vertical Takeoff and Landing (VTOL) and fixed-wing UAVs. In this paper, we present a new design of a tailsitter UAV, named AVALON (Autonomous VerticAL takeOff and laNding). This UAV is composed of typical actuators and is independent of auxiliary infrastructure for vertical takeoff and landing. An autopilot for the tracking control problem of the AVALON vehicle is also proposed to maintain the aircraft in predefined conditions during all flight stages. Simulations results based on the AVALON equations of motion showed that the control techniques applied to all flight stages enable its use as an UAV platform successfully.
引用
收藏
页数：6
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