Enhanced Control Methods for Aerial and Space Vehicles Equipped with Limited Force Actuators

配备有限力执行器的航空航天器的增强控制方法

• 批准号: EP/X012654/1
• 负责人: Matthew Turner
• 金额: $ 31.14万
• 依托单位: University of Southampton
• 依托单位国家: 英国
• 项目类别: Research Grant
• 财政年份: 2022
• 资助国家: 英国
• 起止时间: 2022 至 无数据
• 项目状态: 未结题
• 来源: https://gtr.ukri.org/projects?ref=EP%2FX012654%2F1
• 关键词: Enhanced; Control; Methods; Aerial; Space

This research supports the nation's defense and space programs by providing new methods for controlling aerial and space vehicles, e.g., drones, missiles, rockets, landers, and ascent vehicles. The research also promotes the progress of science by addressing an unresolved issue: aerial and space vehicles have actuators (propellers, control surfaces, thrusters) that can only produce a limited amount of force when maintaining the vehicle's flight path. For example, Martian landers and ascent vehicles are sensitive to unpredictable environmental forces that may prevent them from following their desired trajectory. To counterbalance these forces, the flight control system may have to request thrust commands that exceed the limits of the vehicle's thrusters. The consequence: undesirable flight performance which may hinder the mission. To avoid this, control engineers presently exploit over-sized thrusters at the expense of increased vehicle weight and cost. This research provides control methods that safeguard against this consequence allowing control engineers to design vehicles with smaller sized actuators, hence providing vehicle weight, cost, and scheduling savings. Integrated research, teaching and outreach activities will be carried out through affiliations with university institutes and external centers that foster multidisciplinary collaboration among engineering and other STEM departments, and through collaborations with scholarly organizations that serve historically underrepresented populations. The project will have an impact at the international level through this joint United States/United Kingdom collaboration.

这项研究通过提供控制航空和航天器的新方法来支持国家的国防和太空计划，例如，无人机、导弹、火箭、着陆器和上升飞行器。该研究还通过解决一个尚未解决的问题促进了科学的进步：航空和太空飞行器的执行器（螺旋桨，控制面，推进器）在维持飞行器的飞行路径时只能产生有限的力。例如，火星着陆器和上升飞行器对不可预测的环境力很敏感，可能会阻止它们遵循预期的轨道。为了平衡这些力，飞行控制系统可能不得不请求超过飞行器推进器极限的推力指令。其后果是：飞行性能不佳，可能妨碍使命。为了避免这种情况，控制工程师目前以增加飞行器重量和成本为代价来利用过大的推进器。这项研究提供了控制方法，防止这种后果，使控制工程师设计的车辆与较小尺寸的执行器，从而提供车辆重量，成本和调度节省。综合研究，教学和外展活动将通过与大学机构和外部中心的联系，促进工程和其他STEM部门之间的多学科合作，并通过与服务于历史上代表性不足的人口的学术组织的合作来进行。该项目将通过美国和联合王国的这一联合协作在国际一级产生影响。

项目成果

Model reference adaptive anti-windup compensation

• DOI: 10.1109/cdc51059.2022.9992768
• 发表时间: 2022-12
• 期刊: 2022 IEEE 61st Conference on Decision and Control (CDC)
• 作者: J. Sofrony;M. Turner;C. M. Richards

Anti-windup Compensation for Stable and Unstable Systems with Quantized and Saturated Inputs

具有量化和饱和输入的稳定和不稳定系统的抗饱和补偿

• DOI: 10.23919/acc55779.2023.10156408
• 发表时间: 2023
• 期刊: Proceedings of the American Control Conference
• 作者: Richards, Christopher M.;Turner, Matthew C.
• 通讯作者: Turner, Matthew C.