Add to ORKG提出了一种新的模型直升机航向控制算法。针对具有模型不确定性的直升机航向线性模型,提出了一种具有自适应机制的最优保性能控制器。该控制策略通过引入自适应机制降低固定增益控制器所固有的保守性,并且控制器的反馈增益应用线性矩阵不等式(LMIs)方法解得。理论分析和数字仿真表明所设计的控制器具有良好的鲁棒稳定性能
A new design method of robust guaranteed cost controller with adaptation mechanism was proposed. A l...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
本文提出了利用神经网络学习人手遥控直升机特点的控制方法,针对单一网络进行训练时存在权值相互影响而造成的控制效果不稳定的情况,结合直升机的固有特点,提出了4神经网络的网络结构,降低了训练数据的干扰,改善...
提出了一个新的鲁棒控制方法并将其应用到小型无人直升机的航向控制中.给出了直升机的非线性航向动力学模型并进行简化,然后线性化为具有仿射不确定性的线性模型.针对这个线性模型,基于线性矩阵不等式方法提出了具...
本文着重解决小型无人直升机航向自适应控制问题.通过求非线性函数导数,把原始系统扩展为一个带有伪状态变量的新系统.这种方法不必求解非线性函数的逆,并且降低了计算量.证明了该方法的稳定性.针对实际模型直升...
直升机航向动力学包含输入非线性、时变参数和主-尾旋翼之间的强耦合,传统的比例积分微分(Proportional integral differential,PID)方法很难达到良好的控制性能。基于以上...
直升机航向动力学包含输入非线性、时变参数和主-尾旋翼之间的强耦合,传统的比例积分微分(Proportional integral differential,PID)方法很难达到良好的控制性能。基于以上...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems ...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems ...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems....
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems....
This paper deals with the problem of robust tracking control with adaptation mechanism to improve tr...
This paper deals with the problem of robust tracking control with adaptation mechanism to improve tr...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
A new design method of robust guaranteed cost controller with adaptation mechanism was proposed. A l...
A new design method of robust guaranteed cost controller with adaptation mechanism was proposed. A l...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
本文提出了利用神经网络学习人手遥控直升机特点的控制方法,针对单一网络进行训练时存在权值相互影响而造成的控制效果不稳定的情况,结合直升机的固有特点,提出了4神经网络的网络结构,降低了训练数据的干扰,改善...
提出了一个新的鲁棒控制方法并将其应用到小型无人直升机的航向控制中.给出了直升机的非线性航向动力学模型并进行简化,然后线性化为具有仿射不确定性的线性模型.针对这个线性模型,基于线性矩阵不等式方法提出了具...
本文着重解决小型无人直升机航向自适应控制问题.通过求非线性函数导数,把原始系统扩展为一个带有伪状态变量的新系统.这种方法不必求解非线性函数的逆,并且降低了计算量.证明了该方法的稳定性.针对实际模型直升...
直升机航向动力学包含输入非线性、时变参数和主-尾旋翼之间的强耦合,传统的比例积分微分(Proportional integral differential,PID)方法很难达到良好的控制性能。基于以上...
直升机航向动力学包含输入非线性、时变参数和主-尾旋翼之间的强耦合,传统的比例积分微分(Proportional integral differential,PID)方法很难达到良好的控制性能。基于以上...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems ...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems ...
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems....
This paper discusses the adaptive robust guaranteed cost tracking control problem of linear systems....
This paper deals with the problem of robust tracking control with adaptation mechanism to improve tr...
This paper deals with the problem of robust tracking control with adaptation mechanism to improve tr...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
A new design method of robust guaranteed cost controller with adaptation mechanism was proposed. A l...
A new design method of robust guaranteed cost controller with adaptation mechanism was proposed. A l...
This paper presents a new robust controller design approach to the yaw control of a small-scale heli...
本文提出了利用神经网络学习人手遥控直升机特点的控制方法,针对单一网络进行训练时存在权值相互影响而造成的控制效果不稳定的情况,结合直升机的固有特点,提出了4神经网络的网络结构,降低了训练数据的干扰,改善...