Aerosp. Eng. Dept., Sharif Univ. of Technol., Tehran;
Riccati equations; adaptive control; aerospace safety; aircraft landing guidance; attitude control; control system synthesis; helicopters; level control; position control; remotely operated vehicles; robust control; tracking; 6DOF moving platform; SDRE method; adaptive control system design; autonomous unmanned aerial vehicle; helicopter landing system design; robustness; safe touchdown; state dependent Riccati equation method; tracking level control; Moving platform; automatic landing; unmanned helicopter;
机译:GPS拒绝场景下用于在移动平台上自主降落的无人机直升机相对状态估计
机译:滑行式起落架直升机自动旋转着陆安全性设计系统和实验研究的当代方法
机译:基于模糊逻辑的无人机自主着陆系统设计方法。
机译:自动无人直升机着陆系统设计,用于6dof移动平台的安全触控
机译:无人四旋翼旋翼飞机在运动物体上的自主着陆控制。
机译:基于无人直升机的机载电力线检查系统中多传感器两轴惯性稳定平台复合控制方案的实验验证
机译:考虑到复合体平台的降落,形成直升机型无人曝气线的形成