SAE AIR 1810C:2003
$25.35
Design, Development and Test Criteria – Solid State Proximity Switches/Systems for Landing Gear Applications
Published By | Publication Date | Number of Pages |
SAE | 2003-01-08 | 17 |
This document examines the most important considerations relative to the use of proximity sensing systems for applications on aircraft landing gear. In general, the recommendations included are applicable to other demanding aircraft sensor installations where the environment is equally severe.
Published Code | SAE |
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Published By | SAE International, formerly Society of Automotive Engineers |
Publication Date | 2003-01-08 |
Pages Count | 17 |
Language | English |
Descriptors | Electronic control systems; Electromagnetic compatibility; Landing gear; Fault detection; Sensors and actuators; Mountings; Electronic equipment; Wheel wells; Integrated circuits; Failure modes and effects analysis |
File Size | 870.4 KB |
ICS Codes | 31.200 - Integrated circuits. Microelectronics 33.100 - Electromagnetic compatibility (EMC) 43.040.10 - Electrical and electronic equipment |