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Control failure of the roll-isolated inertial navigation system under large pitch angle 被引量:3
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作者 Jinchao SONG Shuxing YANG Fenfen XIONG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第10期2707-2715,共9页
Roll-isolation is an effective way for spinning vehicle to greatly reduce the roll gyro range of strapdown Inertial Navigation System(SINS)and increase the accuracy of inertial navigation.However,during a recent fligh... Roll-isolation is an effective way for spinning vehicle to greatly reduce the roll gyro range of strapdown Inertial Navigation System(SINS)and increase the accuracy of inertial navigation.However,during a recent flight test,the roll-isolated control system failure was observed under a large pitch angle(706 h 685),which introduces a sharply increase in the roll angular velocity,the saturation of roll gyro and the inertial navigation failure.To address this issue,the governing equation of the roll-isolated system is derived with the consideration of various disturbance factors.The control failure is reproduced by numerical simulation.And the results show that the pitch and yaw angular velocity can cause a dramatic increase in roll rate under the large pitch angle,resulting in the roll-isolated control failure.Meanwhile,an improved roll-isolated control system is developed using PI controller,which is verified by mathematical simulation. 展开更多
关键词 Spinning vehicle Strap-down inertial navigation system(SINS) Roll-isolated control Control failure large pitch angle
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