Shenzhen Nuobashi Trading Co.,Ltd

Features as follows
1 The CPU is powered by NXP POWERPC P1010, with a maximum main frequency of 800MHz
2 DDR3 has a capacity of 1GB, ROM 1GB, NVSRAM 256KB and FLAHS 16Gb*8bit
3 5-channel RS422 interface, 2-channel RS232 interface
4 16-channel discrete input interface, 16-channel discrete output interface (discrete type configurable)
5 8-channel analog input interface, 8-channel analog output interface
6 5-channel PWM output interface
7 1 channel CAN communication interface (reserved)
8 1 channel synchronous input and 1 channel synchronous output interface (reserved)

ProductDescription

ZY8DN04-T1Single Redundant Flight Control Computer is based on the analysis of similar products at home and abroad, and combined with the latest technical development trend as well as the latest needs of users. ZY8DN04-T1 takes NXP's high-performance low-power processor P1010 as its core, supports VxWorks real-time operating system, and provides rich peripheral interfaces, flight parameter recording and other flight control computer proprietary functions. ZY8DN04-T1 is suitable for airborne, shipborne and vehicle-mounted applications in harsh working environments.

WorkingEnvironment

Temperature range........... -10℃～65℃

Relative humidity............. 5﹪～95﹪, nocondensation

Shock vibration................ 5g

General Specification

Case material........... Aviation aluminum alloy

TypicalApplications

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