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
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
相关论文
共 50 条
  • [31] A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
    Pavlov V.V.
    Russian Aeronautics, 2016, 59 (4): : 507 - 516
  • [32] Deep Stall Landing Strategy for Small Fixed-Wing Aircraft Aided by Morphing
    He Zhen
    Kan Yingying
    Li Da
    2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017, : 6772 - 6776
  • [33] Hybrid control strategy for the autonomous transition flight of a fixed-wing aircraft
    Casau, Pedro
    Cabecinhas, David
    Silvestre, Carlos
    IEEE Transactions on Control Systems Technology, 2013, 21 (06) : 2194 - 2211
  • [34] Aerodynamic modeling and performance analysis of model predictive controller for fixed wing vertical takeoff and landing unmanned aerial vehicle
    Getachew, Melkamu Tadesse
    Zeleke, Dinku Seyoum
    ENGINEERING RESEARCH EXPRESS, 2024, 6 (02):
  • [35] Autonomous Landing Control of Fixed-wing UAVs: from Theory to Field Experiment
    Zhang, Daibing
    Wang, Xun
    JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2017, 88 (2-4) : 619 - 634
  • [36] Vision-aided navigation for fixed-wing UAV's autonomous landing
    Zhang, Yelin
    Wang, Yangzhu
    Han, Zhen
    2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 988 - 992
  • [37] Autonomous Landing Control of Fixed-wing UAVs: from Theory to Field Experiment
    Daibing Zhang
    Xun Wang
    Journal of Intelligent & Robotic Systems, 2017, 88 : 619 - 634
  • [38] Autonomous Runway Alignment of Fixed-Wing Unmanned Aerial Vehicles in Landing Phase
    Pouya, Soha
    Saghafi, Fariborz
    ICAS: 2009 FIFTH INTERNATIONAL CONFERENCE ON AUTONOMIC AND AUTONOMOUS SYSTEMS, 2009, : 208 - 213
  • [39] Mathematical simulation of near-vertical flight of fixed-wing aircraft
    Mebius, JE
    JOURNAL OF AIRCRAFT, 1996, 33 (03): : 644 - 647
  • [40] Unmanned Air Vehicle - Autonomous Takeoff and Landing
    Lim, K. L.
    Gitano-Briggs, Horizon Walker
    FOURTH INTERNATIONAL CONFERENCE ON EXPERIMENTAL MECHANICS, 2010, 7522