在执行器有效性丧失和风力扰动下,可变距离四旋翼机的容错控制
Alessandro Baldini1, Riccardo Felicetti1, Alessandro Freddi1
1Department of Information Engineering, Università Politecnica delle Marche, 60131 Ancona, Italy.
Sensors (Basel, Switzerland)
|July 11, 2023
概括
本研究介绍了可变度四旋翼的耐故障控制系统,尽管执行器故障和风力干扰,只使用动力学数据,但能够实现稳健的飞行. 该系统有效地管理故障和环境因素,以实现更安全的空中操作.
科学领域:
- 机器人和控制系统 机器人和控制系统
- 航空航天工程 航空航天工程
- 容错系统 容错系统
背景情况:
- 带有可变调度执行器的四旋翼机面临着执行器故障和外部干扰的挑战.
- 现有的控制方法通常需要复杂的传感器数据,这限制了实际应用.
- 确保在不确定的条件下可靠运行对于自动驾驶飞行器至关重要.
研究的目的:
- 为变速四旋翼机开发一个耐故障控制 (FTC) 策略.
- 用基于模型的方法解决执行器故障和外部风力干扰.
- 为了减少对FTC广泛传感器测量的依赖.
主要方法:
- 使用了基于观察者的干扰控制 (DOBC) 策略.
- 顺序二次编程 (SQP) 用于控制分配.
- 使用了来自惯性测量单元 (IMU) 的动力学数据.
- 在特定条件下,一个观察员处理了执行器故障和风力干扰.
主要成果:
- 拟议的FTC计划成功地管理了多个执行器故障.
- 该系统证明了对风力干扰和测量噪声的稳定性.
- 控制分配有效地处理了变速非线性动力学,推力和速度限制.
- 该方法只需要动态IMU数据,而不是电机转速或电流.
结论:
- 开发的耐故障控制方案能够处理变速四旋翼的执行器故障.
- 这种方法在有风的环境中是有效的,并且对测量噪声有弹性.
- 依赖最小的传感器数据增强了拟议的FTC系统的实用性.
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