首页> 美国政府科技报告 >Development of a Hydrofluidic Vernier Rocket Control System for Ejection Seat Stabilization.
【24h】

Development of a Hydrofluidic Vernier Rocket Control System for Ejection Seat Stabilization.

机译:用于弹射座椅稳定的液压流体游标火箭控制系统的研制。

获取原文

摘要

A feasibility demonstration model of a fluidic thrust vector control (FTVC) system was designed, fabricated, and tested for pitch stabilization of ejection seats using the STAPAC vernier rocket. The control system includes a rate sensor, amplifier, attitude memory, and a position-controlled hydrofluidic servoactuator. The measured dynamic response of the control system closely matched the theoretical specifications for stable attitude control of the seat. The hardware was tested on a hydraulic rate table without rocket firing. (Author)

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号