Collects data from various sensors within the aircraft system, converts it into the required format, and transmits it to the mission computer or flight control computer. Converts control commands received from the mission computer or flight control computer and relays them to sensors and other peripheral devices. Supports system control functions, monitors the status of key systems, and provides feedback. Achieves 70% cost competitiveness compared to equivalent-performance products. - x2 MIL-STD-1553B - x2 UART (RS-422/485) - x24 Analog input interfaces - x8 Analog output interfaces - x64 Discrete input interfaces - x40 Discrete output interfaces - Size : 270 x 270 x 62.2mm - Weight : 2.5Kg - Power : MIL-STD-704F (28VDC, 10W) - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G

The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.

The D56M differential pressure switch provides high precision measurement across a wide range of low-differential pressure conditions in a package smaller than other units of comparable capability. The membrane senses changes between the “high” and “low” pressure inlets while offering excellent repeatability and high cycle life. Optional hermetically sealed contacts mean the D56M can be well suited when vapor ignition is a concern.

Typical uses include airflow control plenums.

For a similar switch with a higher resistance to shock and vibration, refer to the D16M

For qualification information, please consult the sales or engineering departments.

Features

Intended for gaseous media
Environmentally sealed with optional hermetically sealed contacts
Proven diaphragm and leaf spring technology for high cycle life

# Key Features - Map Generation and No-Drive Zone Setting in Airports > Airport map/sensor fusion-based localization function > Function for defining main movement and standby areas > No-drive zone setting - Optimal Path Autonomous Driving Function > Destination-based optimal path navigation > Speed limit settings by path and area > Real-time location monitoring > Obstacle detection and immediate response > Driving on diverse road surfaces within designated areas - Real-Time Bird Detection and Bird Position/Direction Prediction > Real-time bird detection > Support for approximate bird position/direction prediction based on object detection algorithms > Updating of approximate bird position/direction prediction based on flock detection - Effective Bird Deterrence Reflecting Bird Characteristics > Playback of diverse (randomized) acoustic patterns - Real-Time Communication with Operator and Manual Control Function > Monitoring console (PC) provides real-time bird detection status and history > Display of approximate bird position/direction predictions on a map > Real-time video data sharing > Remote manual control - Smart Charging Function > Automatic return and charging when mission is complete or battery is low

The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

Yuan Thor platform serves as the computational core for autonomous systems. Powered by NVIDIA® Jetson Thor™ (128GB LPDDR5X, 2560 CUDA cores, 96 Tensor cores), it delivers up to 2070 FP4 TFLOPS of AI performance for real-time sensor fusion, data analytics, and edge decision-making. Thor supports 16× MIPI CSI-2 cameras, audio in/out, CAN Bus, UART, I²C, SPI, and GPIO, enabling precise, low-latency responses for robotics, industrial automation, and autonomous vehicles.

The device consists of a power supply, dedicated Iridium and GNSS antenna, BLE, three configurable inputs/outputs, RS232, and CANbus in an environmentally sealed enclosure. Includes an Iridium Short Burst Data (SBD) modem that allows remote devices to send and receive satellite messages from anywhere in the world.

• Arinc connectors • Modular connectors • D-sub / Rectangular connectors • Terminal blocks • Quick junction modules