Description
Features as follows
1 ZY 8DN01 Double Redundant Flight Control Computer
2 Provide Micro SD,USB memory interface
3 RS232/422,AD/DA. PWM
4 Embedded inertial navigation unit, differential GPS unit
5 Data link transmitting unit
6 Provide DC 24Voltage output and motor driving module
7 Aluminum alloy profile frame structure
8 The base with a JPMZ-0.5 shock absorber
Product Description
The device is a flight control computer platform applied to UAV with laminated structure of four layers inside, including functions as data processing, data acquisition, communication, long-distance data transmission, direction inertial navigation and so on. It adopts PC104 stack, peripheral module construction realized by external extend device's local bus of embedded processer. This device contains one port of RS232 and one port of RS422, debug interface for JTAG and UART, built-in inertial navigation, barometer, GPS module and a base with JPMZ-0.5 shock absorber. The whole machine frame structure is designed by aviation aluminum alloy-alloy so it has obvious characters of firm construction and light body. It is a flight control computer which integrates aviation control with task to meet the autonomous flight control and mission of the multi-rotatable wings/fixed-wings airplane and helicopter.
Working Environment
Temperature range ……………… -10℃~65℃
Relative humidity …………… 5﹪~95﹪, no condensation
Shock vibration ……………… 5g
General Specifications
External dimensions (L×W×H) (without ear) ……………… 125×150×88 mm
Case material ……………… aviation aluminum alloy
Typical Applications
Construction of automatic testing system
Laboratory automation, research and design verification
Flight control computer, the core of the UAV flight control system, is the solution device of control system to realize the control law calculation function of flight control system and output control command to servo system. Flight controlcomputer is also the management part of all the system, which is responsible for redundancy management calculation, logical judgment, working mode conversion, and achieves the declaration of system state, fault alarm and BIT function of the whole flight control system. It provides signal interfaces from other parts of the system and from the system to the on-board cross-link equipment on the machine and processes the signals.
We can customize redundancy flight control computers according to customers’ demands.
●Achieving redundancy management and self-test function through hardware and software to meet the reliability requirements of flight computer and flight control system reliable.
● According to the information of command sensor and flight movement sensor, it performs control law calculation and the result is input to servo system to control motion of rudder actuator.
● Self-test capability to meet the system testability requirements and providing test circuits for other parts
● Providing power supply for some other external parts
- UAV
- unmanned and accessories
- radar
- hardware
- navigation
- surveillance
- engine
Production Capacity:
Not informed
Delivery Timeframe:
Depends on Size of Order
Incoterms:
Not informedPackaging Details:
Not informed
More about
Shenzhen Nuobashi Trading Co.,Ltd
10-50
Employees
Not informed
100%
% Export sales
Year
Established
Business type
- Industry / Manufacturer
- Distributor / Wholesaler
Keywords
- Semiconductors
- automotive diagnostics
- drones
- oscilloscopes
- electronic components
Contact and location
- Weili Liang
- +86 xxxxxxxx
- 深圳 / | China