ANGULAR PARAMETER PICKUPS OF FLIGHT VEHICLES ON THE BASIS OF THE GYROS WITH A ROTARY GIMBAL SUSPENSION

机译：旋转陀螺悬挂的陀螺仪飞行器角参数曲线

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Angular-movement and velocities pickups of the spinning (with respect to roll) flying vehicle (FV) have been developed. These pickups are built on the principle of a three-degrees of freedom gyroscope featuring a rotary gimbal suspension, the main axis of which is directed along the FV's longitudinal axis. Developmental samples of the pickups were manufactured and the laboratory tests were carried out, which confirmed compliance of the pickups to the requirements of the technical assignment on their development.

机译：已经开发了旋转的（相对于滚动的）飞行器（FV）的角运动和速度传感器。这些拾音器基于具有旋转万向悬架的三自由度陀螺仪的原理构建，其主轴线沿FV的纵轴指向。制造了皮卡的开发样品并进行了实验室测试，这证实了皮卡符合其开发技术任务的要求。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU)》|2004年|P.285-286|共2页
会议地点 Saint Petersburg(RU)
作者
V. N. Belobragin; V. I. Gorin; V. YA. Raspopov;
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作者单位

FSUE 'SPLAV SRPA', Shscheglovskaya Zaseka, Tula, 300004, Russia;

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会议组织
原文格式 PDF
正文语种 eng
中图分类无线电导航;
关键词
three-extent gyroscope; rotary gimbal suspension;

机译：三伸陀螺仪;旋转万向悬架;

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ANGULAR PARAMETER PICKUPS OF FLIGHT VEHICLES ON THE BASIS OF THE GYROS WITH A ROTARY GIMBAL SUSPENSION

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