Satellite inertial navigation combined type missile guidance control system and simulation method

The invention discloses a satellite inertial navigation combined type missile guidance control system, and relates to the technical field of forest fire control, the control system is based on a frame structure of a digital signal processor DSP and a programmable logic device FPGA, and the control s...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	XUAN HAIYING, LI YONGJUN, WANG ZHIQIANG, WANG XUAN, WANG ZHELEI, YAN ZHIYE, GENG LIJIE, ZHU, ZHAONING, GENG LINLIN, LIANG XIAOLE, SHEN YONGMING, LI YADONG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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