aerodynamics; autonomous aerial vehicles; control system synthesis; discrete time systems; linear quadratic control; pitch control (position); three-term control; velocity control; F-16 model; PID controller; aerodynamics; altitude keeping; altitude tracking; discrete-time linear quadratic regulator(DLQR); fixed-wing UAV; fixed-wing unmanned aerial vehicle; flight altitude; flight velocity; inner loop controller; linear model set; linearized models; longitudinal control law design; longitudinal dynamics; multimodel technique; pitch angle control; switching strategy; velocity control; Adaptation models; Adaptive control; Aircraft; Atmospheric modeling; Mathematical model; Switches;
机译:基于PID控制设计的固定翼无人机纵向动力学振动分析。
机译:固定翼无人机纵向飞行动力学改进LQG控制的对比设计
机译:基于PI的固定翼无人机基于控制分配的容错控制
机译:固定翼无人机纵向动力学的多模型控制设计
机译:演示基于集合的设计技术-无人机案例研究
机译:基于UAV形成的区域代理模型技术快速调整PID控制器
机译:固定翼无人机过渡到悬停飞行的自适应控制技术