Spiral descent of an unmanned aerial vehicle

被引:1
作者
Gomzin A.V. [1 ]
Fesenko E.V. [1 ]
Shataev V.G. [2 ]
机构
[1] OAO OKB Sokol, Kazan
[2] Tupolev State Technical University, Kazan
来源
Russian Aeronautics | 2009年 / 52卷 / 03期
关键词
Intensive descent; Investigation; Spiral; Target; Unmanned aerial vehicle;
D O I
10.3103/S1068799809030040
中图分类号
学科分类号
摘要
An intensive unsteady spiral descent of an unmanned aerial vehicle with an approach to target (object) at the design altitude and specified minimal flight speed is considered. The decisive equations describing the motion of the FV center-of-mass are solved by time intervals. The influence of controlling parameters on the spiral radius, the maneuver speed and time is studied. © Allerton Press, Inc., 2009.
引用
收藏
页码:277 / 283
页数:6
相关论文
共 3 条
[1]  
Ostoslavskii I.V., Aerodinamika samoleta (Aircraft Aerodynamics), (1957)
[2]  
Lebedev A.A., Chernobrovkin L.S., Dinamika poleta bespilotnykh letatel'nykh apparatov (Unmanned Aerial Vehicle Flight Dynamics), (1973)
[3]  
Korovin A.E., Novikov Y.F., Prakticheskaya aerodinamika i dinamika poleta samoletov YaK-52 i YaK-55 (Practical Aerodynamics and Flight Dynamics of the Yak-52 and Yak-55 Aircraft), (1989)