摘要
针对某型飞机设计了一套重心自动调节系统.根据飞机结构及飞行时结构变化、燃油消耗等对重心的影响,建立了飞机飞行时重心的数学模型,飞行时实时解算飞机重心,对飞机重心进行实时调节以满足试飞需求.
A kind of plane＇s barycentre control system is designed,which meets the actual needs of flight test for aircraft flight stereotypes.According to the aircraft structure and focus of the factors,the gravity model of aircraft center is established to calculate plane＇s barycentre and analyze the regulation laws.The main ideas of the design are introduced and the hardware as well as the software structure is presented.It has been verified by the ground testing that the system meets the requirements of actual flight mission.
出处
《机械与电子》
2010年第6期38-41,共4页
Machinery & Electronics
