TY - GEN
T1 - Analysis of onboard takeoff and landing characteristics for unmanned aerial vehicles
AU - Liu, Dongxu
AU - Liu, Gang
AU - Hong, Guanxin
N1 - Publisher Copyright:
© 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2016
Y1 - 2016
N2 - Compared to manned aircrafts, UAVs(Unmanned Aerial Vehicles) have their special advantages and irreplaceable functions. Meanwhile, for vehicles, the onboard condition in the aircrafts’ takeoff and landing process is much worse than the condition on the ground. Because of the distance restriction onboard, the measures to improve the UAVs’ takeoff and landing performance are necessary. The vehicles can be helped by kinds of methods, such as the ski-jump board or catapult launch in the takeoff process, arresting cable in the landing process. In this work, according to aircraft dynamical theories, the mathematical models of the ski-jumping takeoff, catapult launching take off and arrested deck-landing process are established, which are the basis of numerical simulation. The influence of primary parameters impacted on takeoff and landing characteristicsis analyzed after simulate calculations. With the analysis of the computational contrast, the measures to modify the parameters and meet the requirement, are concluded.
AB - Compared to manned aircrafts, UAVs(Unmanned Aerial Vehicles) have their special advantages and irreplaceable functions. Meanwhile, for vehicles, the onboard condition in the aircrafts’ takeoff and landing process is much worse than the condition on the ground. Because of the distance restriction onboard, the measures to improve the UAVs’ takeoff and landing performance are necessary. The vehicles can be helped by kinds of methods, such as the ski-jump board or catapult launch in the takeoff process, arresting cable in the landing process. In this work, according to aircraft dynamical theories, the mathematical models of the ski-jumping takeoff, catapult launching take off and arrested deck-landing process are established, which are the basis of numerical simulation. The influence of primary parameters impacted on takeoff and landing characteristicsis analyzed after simulate calculations. With the analysis of the computational contrast, the measures to modify the parameters and meet the requirement, are concluded.
UR - https://www.scopus.com/pages/publications/84985945420
U2 - 10.2514/6.2016-3376
DO - 10.2514/6.2016-3376
M3 - 会议稿件
AN - SCOPUS:84985945420
SN - 9781624104299
T3 - AIAA Modeling and Simulation Technologies Conference, 2016
BT - AIAA Modeling and Simulation Technologies Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Modeling and Simulation Technologies Conference, 2016
Y2 - 13 June 2016 through 17 June 2016
ER -