|
CN112284679A
|
|
Five-component balance for gas vane force measurement and component force calculation method
|
|
CN112284750A
|
|
Method for testing performance of gas rudder of solid rocket engine
|
|
CN112161520A
|
|
Rear cover structure of launch canister and installation and use method
|
|
CN111478418A
|
|
Power conversion and power failure control system and method
|
|
CN111366044A
|
|
Guidance control method for flat flight transition section
|
|
CN111488667A
|
|
Parameterized pneumatic design method of meteorological detection rocket
|
|
CN111427327A
|
|
Protection method for abnormal restart of aircraft control software
|
|
CN111488168A
|
|
Weapon system control software safety upgrading method based on boot secondary loading
|
|
CN111452962A
|
|
Rotor radial locking device and locking method of vertical take-off and landing aircraft
|
|
CN111452961A
|
|
Rotor wing axial locking device and locking method of vertical take-off and landing aircraft
|
|
CN110989557A
|
|
Long-range guided missile test system based on PXI bus
|
|
CN111504142A
|
|
Universal missile simulator and simulation method
|
|
CN111650958A
|
|
Online path planning method for switching in route points of take-off section of fixed-wing unmanned aerial vehicle
|
|
CN111332465A
|
|
Propeller and ducted fan combined type tilt rotor unmanned aerial vehicle and flight mode
|
|
CN111426490A
|
|
Steering engine torque dynamic loading device in full-elastic state and testing method
|
|
CN110794375A
|
|
Novel radar scattering cross section reinforcing device
|
|
CN111263249A
|
|
Telemetry data processing method and device and readable storage medium
|
|
CN111091697A
|
|
Telemetry data processing system
|
|
CN111795617A
|
|
Penetration warhead plug device
|
|
CN110986695A
|
|
Manual switching mechanism for working or testing state of initiating explosive device
|
