摘要
通过反潜直升机吊放声纳控制系统的半实物实时仿真系统研究 ,建立了半实物仿真的结构和直升机与缆绳的数学模型 ,进行了相关硬件设备的研制 ,并编写了实时仿真软件 ,进行了多种条件下的半实物实时仿真研究工作。通过仿真验证了直升机上的吊放声纳飞行控制系统满足性能指标要求 。
This paper studies the real time semi physical simulation of helicopter's sonar cable control system. The mathematical models of helicopter and cable are established and the hardware equipment are manufactured. Finally the real time simulation program is coded and the simulation is fulfilled successfully under various conditions. It's turned out that the sonar control system in the helicopter is well designed and satisfies the requirement. The result of the semi physical simulation is in accordance with the acquired data of real flight test.
出处
《飞行力学》
CSCD
北大核心
2000年第3期72-75,共4页
Flight Dynamics
