CN103383745A
|
|
Welding point quality detection system detection window optimized layout method
|
CN103384373A
|
|
Telemetry and telecontrol method of distributed cluster aircraft system
|
CN103383539A
|
|
Time measuring method based on double-clock system
|
CN103384172A
|
|
Laser wireless energy transfer communication and tracking integrating system and method
|
CN103383545A
|
|
High-speed miniature pulse signal collecting circuit
|
CN103389917A
|
|
SRAM (static random access memory) type FPGA SEU (field programmable gate array single event upset) operation fixing method
|
CN103383425A
|
|
Satellite-borne general power distribution device for high voltage bus and measuring method thereof
|
CN103384145A
|
|
Method for utilizing time window to eliminate pulse per second jitter
|
CN102730204A
|
|
Spacecraft domestic garbage catapult
|
CN102672720A
|
|
Control method for three-joint mechanical arm
|
CN102360305A
|
|
VxWorks operating system scaling and customizing method for aerospace computer
|
CN102509561A
|
|
SRAM (system random access memory) type FPGA (field programmable gate array) configuration area simulated fault injection method
|
CN102508731A
|
|
Fault tolerance starting method of operating system based on RS (Reed-Solomon) coding and decoding
|
CN102508729A
|
|
Error correction method for dynamic refreshing of ROM (read only memory) mapping zone in FRGA (field programmable gate array)
|
CN102357699A
|
|
Tool clamping apparatus for operations of tin-plating and welding leads of wire-welded type components and parts
|
CN102358436A
|
|
Device for realizing spacecraft orbit keeping by utilizing space debris
|