| 1. | Such methods are called inverse methods
这种方法被称为逆方法 |
| 2. | Due to the strong nonlinearity and uncertainty factors , based on the idea of zeroing normal speeds of los ( line of sight ) , a robust terminal guidance law is designed by the method of dynamic inversion
针对方程中的强非线性因素和不确定因素，基于零化导弹目标视线转率的思想，应用动态逆方法设计了鲁捧的末制导律。 |
| 3. | First give the elementary knowledge of adaptive inverse , then give the construction of filter which is proper to adaptive inverse , and lms adaptive algorithm . the policy is used in the system control , and an achieving way in the design of nonlinear plant is proposed
介绍了自适应逆控制的基本原理，以及适用于自适应逆控制的wiener滤波器结构和自适应lms算法，并将自适应逆方法应用于线性和非线性控制系统中。 |
| 4. | The computer simulation results verify the validity of two adaptive algorithms applied to circular array . the algorithms are least square based on qr decompose ( qrd - ls ) and sampling matrix inversion based on qr decompose ( qrd - smi ) . then we apply circular array with wideband signal
其次,验证了基于qr分解的最小二乘算法( qrd - ls )和基于qr分解的采样矩阵求逆方法( qrd - smi )两种自适应算法在均匀圆阵中的有效性。 |
| 5. | In this dissertation the control loop of attitude angle and collective piston loop are separately . the controller is designed at two scales . and the simulation shows the uncoupling of three attitudes angle loop is achieved with dynamic inversion scheme
在姿态角通道的设计中，采用了动态逆思想，按照时标分离的原则将直升机飞控系统划分为快慢回路，并采用动态逆方法对飞行控制系统进行设计和仿真，仿真结果表明动态逆在通道解耦方面非常有效。 |
| 6. | Based on the equilibrium equation , the states of self - stress and the modes of inextensional mechanisms are solved by the singular value decomposition method . and the equilibrium equation can be solved by the generalized inverse method . the force density method is proposed
在建立空间杆件体系平衡方程的基础上，采用广义逆方法求解各种情况下的平衡方程，采用奇异值分解方法求解索杆的机构位移模态和自应力模态，并推导了力密度方法的基本公式。 |
| 7. | This thesis combines artificial neural networks ( nn ) with adaptive inverse control ( nnai ) on the basis of analyzing their principle and characteristics , and applies them in the control of nonlinear system . an application in the design of automatic landing is shown
本文在深入分析了神经网络和自适应逆方法的原理与特点的基础上，将神经网络与自适应逆方法相结合，着重研究了将这种方法应用于非线性系统的控制问题，最后，用飞机自动着陆的过程，验证了神经网络自适应逆方法的效果。 |
| 8. | For researching the flight test techniques of thrust vector controlled aircraft , dynamic models of thrust vector controlled aircraft were established , four post stall maneuver control laws were designed with the dynamic inverse method , tested and investigated according to a standard evaluation maneuver set ( stems )
摘要为研究推力矢量飞机的试飞技术，建立了推力矢量飞机的动力学模型，用动态逆方法设计了4种过失速机动控制律，并在地面飞行模拟器上参考标准评估机动动作集( stems )进行了飞行模拟试验研究。 |
