Synthetic Wind Estimation for Small Fixed-Wing Drones

被引:1
|
作者
Sharma, Aman [1 ]
Laupre, Gabriel Francois [1 ]
Longobardi, Pasquale [1 ]
Skaloud, Jan [1 ]
机构
[1] Ecole Polytech Fed Lausanne EPFL, Lab Cryospher Sci CRYOS, Environm Sensing Observ, Route Ronquos 86, CH-1950 Sion, Switzerland
基金
欧盟地平线“2020”;
关键词
extended Kalman filter; aerodynamics; fixed-wing drone; delta-wing drone; wind; MODEL-BASED NAVIGATION; UNMANNED AIRCRAFT; VEHICLE; TURBULENCE; SYSTEM; TEMPERATURE; OBSERVER; UAV;
D O I
10.3390/atmos15111339
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
Wind estimation is crucial for studying the atmospheric boundary layer. Traditional methods such as weather balloons offer limited in situ capabilities; besides an Air Data System (ADS) combined with inertial measurements and satellite positioning is required to estimate the wind on fixed-wing drones. As pressure probes are an important constituent of an ADS, they are susceptible to malfunctioning or failure due to blockages, thus affecting the capability of wind sensing and possibly the safety of the drone. This paper presents a novel approach, using low-fidelity aerodynamic models of drones to estimate wind synthetically. In our work, the aerodynamic model parameters are derived from post-processed flight data, in contrast to existing approaches that use expensive wind tunnel calibration for identifying the same. In sum, our method integrates aerodynamic force and moment models into a Vehicle Dynamic Model (VDM)-based navigation filter to yield a synthetic wind estimate without relying on an airspeed sensor. We validate our approach using two geometrically distinct drones, each characterized by a unique aerodynamic model and different quality of inertial sensors, altogether tested across several flights. Experimental results demonstrate that the proposed cross-platform method provides a synthetic wind velocity estimate, thus offering a practical backup to traditional techniques.
引用
收藏
页数:24
相关论文
共 50 条
  • [21] Automatic terminal guidance for small fixed-wing unmanned aerial vehicles
    Yang, Yachao
    Li, Jie
    Liu, Chang
    Yang, Yu
    Li, Juan
    Wang, Zhenbei
    Wu, Xueyong
    Fu, Lei
    Xu, Xiao
    JOURNAL OF FIELD ROBOTICS, 2023, 40 (01) : 3 - 29
  • [22] The attitude control of fixed-wing MAVS in turbulent environments
    Mohamed, Abdulghani
    Massey, Kevin
    Watkins, Simon
    Clothier, Reece
    PROGRESS IN AEROSPACE SCIENCES, 2014, 66 : 37 - 48
  • [23] Aerodynamic efficiency and performance enhancement of fixed-wing UAVs
    Panagiotou, P.
    Yakinthos, K.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 99
  • [24] Directional Axis Estimation including Wind Velocity for Fixed Wing UAV
    Chanhong Park
    Sanghyuk Park
    International Journal of Aeronautical and Space Sciences, 2021, 22 : 995 - 1003
  • [25] Directional Axis Estimation including Wind Velocity for Fixed Wing UAV
    Park, Chanhong
    Park, Sanghyuk
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2021, 22 (04) : 995 - 1003
  • [26] Design and testing of fixed-wing MAVs
    Lin, Jih-Lung
    Wei, Chin-Yi
    Lin, Chi-Yu
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (04) : 346 - 351
  • [27] BOREAL-A Fixed-Wing Unmanned Aerial System for the Measurement of Wind and Turbulence in the Atmospheric Boundary Layer
    Alaoui-Sosse, Sara
    Durand, Pierre
    Medina, Patrice
    Pastor, Philippe
    Gavart, Michel
    Pizziol, Sergio
    JOURNAL OF ATMOSPHERIC AND OCEANIC TECHNOLOGY, 2022, 39 (03) : 387 - 402
  • [28] Ground Plane Estimation for Obstacle Avoidance During Fixed-Wing UAV Landing
    Peszor, Damian
    Wojciechowski, Konrad
    Szender, Marcin
    Wojciechowska, Marzena
    Paszkuta, Marcin
    Nowacki, Jerzy Pawel
    INTELLIGENT INFORMATION AND DATABASE SYSTEMS, ACIIDS 2021, 2021, 12672 : 454 - 466
  • [29] Electrical Launch Catapult and Landing Decelerator for Fixed-Wing Airborne Wind Energy Systems
    Mueller, Johannes Alexander
    Elhashash, Mostafa Yasser Mostafa Khalil
    Gollnick, Volker
    ENERGIES, 2022, 15 (07)
  • [30] Autopilot for Landing Small Fixed-Wing Unmanned Aerial Vehicles with Optical Sensors
    Trittler, Martin
    Rothermel, Thomas
    Fichter, Walter
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (09) : 2011 - 2021