摘要
针对直升机飞行控制的特点 ,结合国际直升机界的研究热点 ,提出了直升机飞行控制的快速原型设计方法。该方法充分利用当今计算机领域的最新技术 ,在不牺牲系统性能的前提下 ,以最低的成本、最快的速度 ,构建最小规模的实时仿真系统和直观的控制系统设计界面 。
The helicopter flight control system is a complicated project characterized by large investment, long period and high risk. This paper proposes the rapid prototype design for helicopter flight control system according to the latest research hotspot. The methodology makes full use of current improvement in computer technology. A mini scale,high speed real time simulation system can be made with the lowest investment without any loss of system performance. The simulation environment can provide both intuitive interface and verification / validation to control system design.
出处
《飞行力学》
CSCD
2002年第1期5-9,共5页
Flight Dynamics
关键词
直升机
飞行控制
快速原型设计
实时仿真
helicopter
flight control
rapid prototype
real time simulation
