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Dynamics Mutation and Tracking Control of Quadrotors under Multiple Operating Conditions

机译:多工况下四旋翼的动力突变和跟踪控制

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This paper presents a systematic study on the important characteristics of linearized quadrotor system models: the interactor matrix and associated high-frequency gain matrix, which are key information for the design of a model reference adaptive control (MRAC) scheme. The paper derives linearized models and transfer matrices at typical operating conditions of a nonlinear quadrotor system. It is discovered that such models belong to two typical groups: one group with a uniform diagonal interactor matrix and the other group with different non-diagonal parameter-dependent interactor matrices. It is also shown that with realistic conditions on the attitude of the quadrotor, the pattern of the signs of the leading principal minors of the high-frequency gain matrices in both groups is fixed, known and non-zero. For the design of a MRAC scheme (which needs a uniform interactor matrix) for all typical operating conditions, an input compensation technique is studied for the quadrotor model and a desired input compensator is designed to assure a uniform interactor matrix. Finally, an adaptive control framework is proposed for a quadrotor at multiple operating conditions.
机译:本文对线性化四旋翼系统模型的重要特征进行了系统的研究:相互作用器矩阵和相关的高频增益矩阵,这是设计模型参考自适应控制(MRAC)方案的关键信息。本文推导了非线性四旋翼系统典型工作条件下的线性化模型和传递矩阵。发现这种模型属于两个典型的组:一组具有统一的对角相互作用体矩阵,而另一组具有不同的非对角参数相关的相互作用体矩阵。还表明,在四旋翼姿态的实际条件下,两组中高频增益矩阵的前导次要符号的符号模式是固定的,已知的和非零的。对于针对所有典型操作条件的MRAC方案(需要统一的交互矩阵)的设计,针对四旋翼模型研究了一种输入补偿技术,并设计了一种所需的输入补偿器以确保统一的交互矩阵。最后,针对四转子在多种工况下提出了一种自适应控制框架。

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