Manned escape aircraft low-altitude wind field detection control system and control method
The invention provides a manned escape aircraft low-altitude wind field detection control system and a control method, and belongs to the technical field of spaceflight launch. The detection control system comprises ground test launch control equipment, a fault detection processing subsystem, an esc...
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creator | WANG JUNFENG JING MUCHUN HUANG CHEN CHENG XING YANG NAN LIU QIAOZHEN YUE WEI QIAN HANG MA LI MA ZONGRUI LI WENQING SONG JING YUE XIAOFEI XU SHANSHAN RONG YI WANG HAITAO SU XIAOFENG CUI YINGWU LIU FENG WANG XIAOPENG QIN TONG ZHANG ZHI XU ZHEYAO GU MINGKUN WANG ZHIPING HAN YUTONG CHANG WUQUAN MENG QINGFENG HAO JINJIE |
description | The invention provides a manned escape aircraft low-altitude wind field detection control system and a control method, and belongs to the technical field of spaceflight launch. The detection control system comprises ground test launch control equipment, a fault detection processing subsystem, an escape control subsystem and an escape system initiating explosive device, wherein the ground test launch control equipment and the fault detection processing subsystem are connected with the escape control subsystem through a plug-off, the plug-off comprises a T power supply signal, a rocket-ground RS422 communication data line and a B power supply signal, the T power supply signal is connected to the escape control subsystem, the rocket-ground RS422 communication data line is simultaneously connected to the fault detection processing subsystem and the escape control subsystem, the B power supply signal is connected to the fault detection processing subsystem, and an instruction signal and RS422 escape parameters are |
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The detection control system comprises ground test launch control equipment, a fault detection processing subsystem, an escape control subsystem and an escape system initiating explosive device, wherein the ground test launch control equipment and the fault detection processing subsystem are connected with the escape control subsystem through a plug-off, the plug-off comprises a T power supply signal, a rocket-ground RS422 communication data line and a B power supply signal, the T power supply signal is connected to the escape control subsystem, the rocket-ground RS422 communication data line is simultaneously connected to the fault detection processing subsystem and the escape control subsystem, the B power supply signal is connected to the fault detection processing subsystem, and an instruction signal and RS422 escape parameters are</abstract><oa>free_for_read</oa></addata></record> |
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subjects | CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING |
title | Manned escape aircraft low-altitude wind field detection control system and control method |
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