利用GPS遥控链路的天基停飞系统

本文研究了利用L波段遥控专利方案实现基于GPS靶场的真正综合式靶场测量系统必须解决的问题。着重讨论硬件及从单音调制遥控系统变换成采用加密和扩频的数字系统需解决的问题。还将谈到将该系统纳入美国空军靶场标准化和自动化(RAS)结构作为一种可能的GPS靶场方案所需费用和时间安排的一些想法,并讨论如果采用该方法将带来比现用系统的优越之处。     

AN EXPERIMENTAL STUDYOF ROTOR AERODYNAMICS IN GROUNDEFFECT AT LOW SPEEDS

Results of an experimental study of the aerodynamics of a helicopter rotor in ground . effect at low speeds are presented in this paper. Experiments of rotor wake flow visualization and induced velocity measurement near the rotor disc were conducted. At some advance ratio, the forward part of the rotor wake, after impinging on the ground, rolls up and recirculates near the rotor leading edge and large increase in induced velocity appears near the rotor leading edge. When the advance ratio increases, the rolled-up wake develops into a concentrated vortex, ground vortex, under the rotor, and the induced velocity near the rotor leading edge becomes much smaller. The ground vortex diminishes as the advance ratio further increases. Recirculation and ground vortex occur in a very narrow region of the advance ratio. These results explain the irregular variations of rotor forces and moments with advance ratio reported in previous works.