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An adaptive actuator failure compensation scheme for landing of a helicopter with robotic legs

机译:一种自适应致动器故障补偿方案,用于与机械腿降落直升机

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This paper develops an adaptive actuator failure compensation scheme for landing of a helicopter with robotic legs. The adaptive control design uses an integration of multiple failure compensator controllers designed for each actuator failure pattern. Such a design effectively utilizes the actuation redundancy of the robotic manipulators, using for landing of a helicopter, to compensate for possible actuator failures with no knowledge of actuator failure pattern, failure time instant and failure values. With complete parameterization of system and actuator failure uncertainties and direct adaptation of controller parameters, the adaptive control scheme guarantees desired closed-loop stability and asymptotic output tracking, despite uncertain actuator failures. Simulation results are presented to verify the desired system performance.
机译:本文开发了一种自适应致动器故障补偿方案,用于用机械腿降落直升机。自适应控制设计使用为每个执行器故障模式设计的多个故障补偿器控制器的集成。这种设计有效利用机器人操纵器的致动冗余,用于使用直升机的着陆,以补偿可能的致动器故障,不知道致动器故障模式,故障时间瞬间和故障值。通过完整的系统和执行器故障的参数化和控制器参数的直接调整,自适应控制方案尽管执行器故障不确定,但自适应控制方案可确保所需的闭环稳定性和渐近输出跟踪。提出了仿真结果以验证所需的系统性能。

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