H∞ control; aerospace control; control system synthesis; linear parameter varying systems; nonlinear control systems; open loop systems; position control; projectiles; H∞ loop-shaping design; autopilot design; canard-guided spin-stabilized projectile; load factor feedback signal; nonlinear model; nose-mounted course correction fuse; open-loop dynamics; pitch-yaw dynamics modeling; q-LPV model; sensor position influence; Aerodynamics; Atmospheric modeling; Computational modeling; Load modeling; Mathematical model; Projectiles; Robustness; Autopilot Design; Flight Mechanics; Gain-scheduling; Guided Projectile; LPV Systems; Robust Control; Sensor Location;
机译:具有不稳定性保护的自旋稳定弹丸的冲击点模型预测控制
机译:房间建模和传感器位置对可变风量控制系统性能评估的影响
机译:步进电机控制和摩擦模型对复杂机械系统精确定位的影响
机译:155mm自旋稳定的Canard制导弹丸的两种H
机译:装有旋转内部零件的射弹的动态建模,控制和线性理论。
机译:测量量混合比和传感器精度对坡度控制模型实时协调的影响研究
机译:子块位置对使用原位相机校准和激光雷达控制点进行集成传感器方向的影响