Robust Design of Transition Flight Control System with Input Constraint

机译：具有输入约束的过渡飞行控制系统的鲁棒设计

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

This paper proposed a new flight control system for transition flight of fixed-wing unmanned aerial vehicle (UAV). Robust controllers are designed for translational motion and rotational motion of a small fixed-wing UAV. Each nonlinear equation is linearized by using dynamic inversion method in the translational and the rotational control systems. An observer based on disturbance accommodating control methodologies and extended Kalman filter are treated to estimate nonlinear terms and state variables of a UAV dynamic system, respectively. We apply the anti-windup control to the control system so as to implement input saturation that might result in system instability. Numerical and flight test results showed that a developed UAV was stably controlled without the saturation during transition flight.

机译：本文提出了一种用于固定翼无人机飞行过渡的新型飞行控制系统。鲁棒控制器设计用于小型固定翼无人机的平移运动和旋转运动。在平移和旋转控制系统中，通过使用动态反演方法将每个非线性方程线性化。基于干扰适应控制方法和扩展卡尔曼滤波器的观察者分别被用来估计无人机动态系统的非线性项和状态变量。我们将防饱和控制应用于控制系统，以实现可能导致系统不稳定的输入饱和。数值和飞行试验结果表明，研制的无人机在过渡飞行过程中得到了稳定的控制，没有饱和。

著录项

来源
《AIAA guidance, navigation, and control conference;AIAA SciTech forum》|2015年|2866-2876|共11页
会议地点
作者
Ryota Hatori; Kenji Uchiyama;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类
关键词

相似文献

外文文献
中文文献
专利

1. Robust adaptive constrained backstepping flight controller design for re-entry reusable launch vehicle under input constraint: [J] . Qin Zou, Fang Wang, Lianghua Zou, Advances in Mechanical Engineering . 2015,第9期

机译：输入约束下可重入可重复使用运载火箭的鲁棒自适应约束后推飞行控制器设计：
2. Stable robust feedback control system design for unstable plants with input constraints using robust right coprime factorization [J] . Deng M, Inoue A, Yanou A International Journal of Robust and Nonlinear Control . 2007,第18期

机译：具有鲁棒右互质分解的具有输入约束的不稳定工厂的稳定鲁棒反馈控制系统设计
3. Robust Finite-Time H_∞ Controller Design for Uncertain One-Sided Lipschitz Systems with Time-Delay and Input Amplitude Constraints [J] . Gholami Hadi, Binazadeh Tahereh Circuits, systems, and signal processing . 2019,第7期

机译：具有时间和输入振幅约束的不确定单侧Lipschitz系统的鲁棒有限时间H_∞控制器设计
4. Robust Design of Transition Flight Control System with Input Constraint [C] . Ryota Hatori, Kenji Uchiyama AIAA guidance, navigation, and control conference . 2015

机译：过渡飞行控制系统的鲁棒设计与输入约束
5. Control design for a class of unstable nonlinear systems with input constraint. [D] . Yang, Pai-Hsueh. 1998

机译：一类具有输入约束的不稳定非线性系统的控制设计。
6. Nonlinear Robust Adaptive Multi-Modal Vibration Control of Bi-Electrode Micro-Switch with Constraints on the Input [O] . Mohsen Mohammadi, Mohammad Eghtesad, Hossein Mohammadi, 2017

机译：输入受限的双电极微动开关的非线性鲁棒自适应多模态振动控制
7. Robust adaptive constrained backstepping flight controller design for re-entry reusable launch vehicle under input constraint [O] . Qin Zou, Fang Wang, Lianghua Zou, 2015

机译：输入约束下再入式可重复使用运载火箭的鲁棒自适应约束反推飞行控制器设计
8. Applications of Eigenstructure Assignment to Design of Robust MIMO (Multi Input Multi Output) Decoupling Controllers and to Reconfiguration Algorithms for Damaged Flight Control Systems [R] . Gavito, V. F. 1986

机译：特征结构分配在鲁棒mImO（多输入多输出）解耦控制器设计中的应用及损伤飞行控制系统的重构算法

Robust Design of Transition Flight Control System with Input Constraint

摘要

著录项

相似文献

相关主题

期刊订阅