|
CN110823380A
|
|
Method and device for inverting target infrared radiation image based on measured data
|
|
CN110727209A
|
|
NDB antenna tuning system with preemptive logic of who controls
|
|
CN110789734A
|
|
Helicopter rotor deformation and flapping angle measuring method and device
|
|
CN110942227A
|
|
Verification method and device for ground support equipment of civil aircraft
|
|
CN110968295A
|
|
Design method of software architecture of test flight real-time monitoring system
|
|
CN110956280A
|
|
Civil aircraft maintenance program verification method
|
|
CN110909417A
|
|
Multi-BOM construction and conversion method for testing and refitting stages in civil aircraft test flight
|
|
CN110991793A
|
|
Aviation security equipment identification resource allocation method
|
|
CN110969336A
|
|
Design method and device for human factor verification scene of civil aircraft maintenance program
|
|
CN110816877A
|
|
Real-time analysis system for pneumatic servo elasticity of airplane
|
|
CN110823431A
|
|
Hinge moment measuring method of movable control surface driven by return connecting rod
|
|
CN110816878A
|
|
Undercarriage loading false wheel with simulation bearing support
|
|
CN110824460A
|
|
Continuous casting piece cabin-out speed real-time measurement method and device
|
|
CN110715612A
|
|
Helicopter rotor deformation and flapping angle measuring method and device
|
|
CN110611676A
|
|
Synchronous and asynchronous data fusion coding device based on IRIG-106 standard
|
|
CN110686066A
|
|
Transmission system and gear strain measuring point acquisition method
|
|
CN110689763A
|
|
Airborne auxiliary navigation method, device and system based on wireless reception
|
|
CN110646099A
|
|
Method and device for inverting target infrared radiation image based on measured data
|
|
CN110686556A
|
|
Method and device for designing size of trial flight and fitting target of laser-guided missile
|
|
CN110662121A
|
|
Decoding device based on IRIG-106 standard
|
