论文标题
统一的控制器，用于起飞和降落的固定翼飞机
Unified controller for take-off and landing for a fixed-wing aircraft
论文作者
论文摘要
起飞和着陆是飞机飞行的最重要的操作。小型固定翼飞机的部署通常是手工制造的，但是当有效载荷增加时，起飞和降落操作时，将在跑道上进行降落操作，从而使过程更加复杂。因此，我们解决了两个操纵的性能，以便使用反馈控制技术开发独特的控制器。我们介绍了纵向飞机动力学，以建模起飞和着陆，考虑到通过摩擦模型的地面滚动力的滚动阻力。我们还介绍了此类模型的控制器设计。进行了稳定性证明，以通过开发的控制法验证系统的稳定性。此外，进行模拟以证实控制定律有效地应用于提出的动态模型。
Take-off and landing are the most important maneuvers for an aircraft's flight. Deployment for small fixed-wing aircraft is usually made by hand but when payload increases, take-off, and landing maneuvers are then performed on a runway making the procedures more complex. For that reason, we address the performance of the two maneuvers in order to develop a unique controller using the feedback control technique. We present the longitudinal aircraft dynamics to model the take-off and landing considering the rolling resistance forces during ground roll through a friction model. We also present the controller design for such a model. A stability proof is conducted to validate the stability of the system with the developed control law. Additionally, simulations are carried out to corroborate that the control law is effective applied to the dynamic model presented.
