发电机组的一次调频控制回路中由于数字电液调节系统与机械液压调节系统的并存,使得本应发挥高灵敏度作用的 DEH 调节系统中设置了和机械液压机组相同的调频死区。考虑到调频死区这一非线性环节的存在使二次调频回路中控制器的受控对象...发电机组的一次调频控制回路中由于数字电液调节系统与机械液压调节系统的并存,使得本应发挥高灵敏度作用的 DEH 调节系统中设置了和机械液压机组相同的调频死区。考虑到调频死区这一非线性环节的存在使二次调频回路中控制器的受控对象发生了改变,因此需要用相应的非线性控制的方法来选择二次调频控制回路中的 PI 控制器的参数。该文研究了调频死区对二次调频回路中的 PI 控制器的受控对象特性的影响,用 Popov 稳定判据作为选择 PI 参数使系统稳定的数学工具,讨论了 PI 参数的变化对系统频率控制质量的影响。展开更多
The experimental data obtained from yaw-roll coupled wind tunnel tests are used for lateral-directional departure prediction,by linearizing the_b model to extract nominal dynamic derivatives at each coupling ratio.The...The experimental data obtained from yaw-roll coupled wind tunnel tests are used for lateral-directional departure prediction,by linearizing the_b model to extract nominal dynamic derivatives at each coupling ratio.The prediction results are compared with those of the existing engineering methods which are based on the conventional aerodynamic derivatives.The comparison shows that the yaw-roll coupling ratio has a great influence on the departure susceptibility.The departure resistance will loss in partial region of the coupling ratio when the angle of attack is higher than a critical value.According to the stable and unstable regions of coupling ratio,a two-segment stability augmentation system with two different feedback gain matrices is obtained by pole-placement method.The two-segment stability augmentation system is used in the simulations of straight and level flight,steady turn,spin recovery and Herbst maneuver.The simulation results are also compared with the applications of a fixed-gain stability augmentation system designed by the conventional aerodynamic derivatives.When the yaw-roll coupling effects are fully considered,the two-segment stability augmentation system is more effective for departure restraint and can provide a better flying quality with less control energy.展开更多
文摘发电机组的一次调频控制回路中由于数字电液调节系统与机械液压调节系统的并存,使得本应发挥高灵敏度作用的 DEH 调节系统中设置了和机械液压机组相同的调频死区。考虑到调频死区这一非线性环节的存在使二次调频回路中控制器的受控对象发生了改变,因此需要用相应的非线性控制的方法来选择二次调频控制回路中的 PI 控制器的参数。该文研究了调频死区对二次调频回路中的 PI 控制器的受控对象特性的影响,用 Popov 稳定判据作为选择 PI 参数使系统稳定的数学工具,讨论了 PI 参数的变化对系统频率控制质量的影响。
基金supported by the National Natural Science Foundation of China(No.11872209)
文摘The experimental data obtained from yaw-roll coupled wind tunnel tests are used for lateral-directional departure prediction,by linearizing the_b model to extract nominal dynamic derivatives at each coupling ratio.The prediction results are compared with those of the existing engineering methods which are based on the conventional aerodynamic derivatives.The comparison shows that the yaw-roll coupling ratio has a great influence on the departure susceptibility.The departure resistance will loss in partial region of the coupling ratio when the angle of attack is higher than a critical value.According to the stable and unstable regions of coupling ratio,a two-segment stability augmentation system with two different feedback gain matrices is obtained by pole-placement method.The two-segment stability augmentation system is used in the simulations of straight and level flight,steady turn,spin recovery and Herbst maneuver.The simulation results are also compared with the applications of a fixed-gain stability augmentation system designed by the conventional aerodynamic derivatives.When the yaw-roll coupling effects are fully considered,the two-segment stability augmentation system is more effective for departure restraint and can provide a better flying quality with less control energy.
