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Autonomous formation flight of helicopters: Model predictive control approach.

机译:直升机的自动编队飞行:模型预测控制方法。

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摘要

Formation flight is the primary movement technique for teams of helicopters. However, the potential for accidents is greatly increased when helicopter teams are required to fly in tight formations and under harsh conditions. This dissertation proposes that the automation of helicopter formations is a realistic solution capable of alleviating risks. Helicopter formation flight operations in battlefield situations are highly dynamic and dangerous, and, therefore, we maintain that both a high-level formation management system and a distributed coordinated control algorithm should be implemented to help ensure safe formations.; The starting point for safe autonomous formation flights is to design a distributed control law attenuating external disturbances coming into a formation, so that each vehicle can safely maintain sufficient clearance between it and all other vehicles. While conventional methods are limited to homogeneous formations, our decentralized model predictive control (MPC) approach allows for heterogeneity in a formation. In order to avoid the conservative nature inherent in distributed MPC algorithms, we begin by designing a stable MPC for individual vehicles, and then introducing carefully designed inter-agent coupling terms in a performance index. Thus the proposed algorithm works in a decentralized manner, and can be applied to the problem of helicopter formations comprised of heterogenous vehicles.; Individual vehicles in a team may be confronted by various emerging situations that will require the capability for in-flight reconfiguration. We propose the concept of a formation manager to manage separation, join, and synchronization of flight course changes. The formation manager accepts an operator's commands, information from neighboring vehicles, and its own vehicle states. Inside the formation manager, there are multiple modes and complex mode switchings represented as a finite state machine (FSM). Based on the current mode and collected information, the FSM generates discrete reference points in state space. Then, the reference trajectory generator makes smooth trajectories from discrete reference points using interpolation and/or an online optimization scheme. By modifying the reference trajectory and triggering mode changes, the formation manager can override behaviors of the MPC controller.; When a vehicle outside of the formation approaches a vehicle at the edge of the formation, the motion of the vehicle at the formation edge acts like a disturbance with respect to the vehicle attempting to join the formation. The vehicle at the edge of the formation cannot cooperate with any vehicle outside of the formation due to constraints on maintaining the existing formation. (Abstract shortened by UMI.)
机译:编队飞行是直升机团队的主要运动技术。但是,当要求直升机团队以严密的编队和恶劣的条件飞行时,发生事故的可能性大大增加。本文提出,直升机编队自动化是一种能够减轻风险的现实解决方案。直升机在战场上的编队飞行操作是高度动态且危险的,因此,我们认为应同时实施高级编队管理系统和分布式协调控制算法,以确保安全编队。安全的自主编队飞行的起点是设计一种分布式控制律,以减弱进入编队的外部干扰,从而使每架飞行器都能安全地保持其与所有其他飞行器之间的间隙。尽管常规方法仅限于均质地层,但我们的分散模型预测控制(MPC)方法允许地层中的异质性。为了避免分布式MPC算法固有的保守性,我们首先为各个车辆设计一个稳定的MPC,然后在性能指标中引入精心设计的代理间耦合项。因此,所提出的算法以分散的方式工作,并且可以应用于由异构车辆组成的直升机编队的问题。团队中的各个车辆可能会遇到各种新出现的情况,这些情况将需要在飞行中进行重新配置的能力。我们提出了编队管理器的概念,用于管理航路变更的分离,合并和同步。编队管理器接受操作员的命令,来自相邻车辆的信息及其自身的车辆状态。在编队管理器内部,有多种模式和复杂模式切换,表示为有限状态机(FSM)。基于当前模式和收集的信息,FSM在状态空间中生成离散参考点。然后,参考轨迹生成器使用插值和/或在线优化方案从离散参考点绘制平滑轨迹。通过修改参考轨迹和触发模式更改,编队管理器可以覆盖MPC控制器的行为。当地层外部的车辆在地层的边缘处接近车辆时,在地层边缘处的车辆的运动就像对试图加入地​​层的车辆的干扰一样。由于维护现有地层的限制,位于地层边缘的车辆无法与地层外部的任何车辆配合。 (摘要由UMI缩短。)

著录项

  • 作者

    Chung, Hoam.;

  • 作者单位

    University of California, Berkeley.;

  • 授予单位 University of California, Berkeley.;
  • 学科 Engineering Aerospace.; Engineering System Science.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 133 p.
  • 总页数 133
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;系统科学;
  • 关键词

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