Disclosed is a landing gear system controller for controlling a landing gear system of an aircraft. The controller is configured to receive a request to operate a non-landing gear system element of the aircraft, and to cause operation of at least part of the landing gear system of the ...
This invention relates to the control of the landing gear of aircraft, and more particularly to a system for automatically positioning the landing gear in accordance with certain flight indications. ' One of the hazards of flight in craft with retractable landing gear has been the possibility......
Brake Control Landing Gear Systems Hydro-Aire Antiskid Systems Brake by Wire Systems Integrated Brake Temperature Monitoring System Integrated SmartStem Wireless Tire Pressure System Brake Control Systems F-16 Brake Control System Redesign Landing Gear Control Systems ...
Kavlico’s Landing Gear Control Lever. (LGCL) provides all the necessary elements for control while providing signal indication via a series of internal control switches. Our Landing Gear Control (LGC) unit meets the small envelope, minimum weight, and high reliability demanded by the aerospace ...
Landing gear extension and retraction systems A portfolio of innovative and performing solutions Safran Landing Systems extension and retraction systems feature a large number of best in class equipments (hydraulic, electric, electronics), integrated with proprietary software algorithms, for unrivalled answers...
Open the forward access door near the nose landing gear. 打开前起落架附近的前接近门. 来自期刊摘选 5. UAV, landing gear, engine, mission equipment, fuel systems, environmental control systems are monitoring targets. 无人机 、 起落架 、 发动机 、 任务设备 、 燃油系统 、 环控系统等是被监控对...
This paper presents experiences in using several model checking tools to verify properties of a critical real time embedded system. The tools we tested are Lesar, SMV, Prover Plug In for SCADE and Uppaal. The application is the landing gear control system of a military aircraft, developed by ...
A semi-active control system of a landing gear suspension can solve the problem of excessive vibrations effectively by providing a variable damping during each operational phase. Magnetorheological (MR) dampers are one of the most efficient and attractive solutions that can provide the continuously ...
A hydraulic control system for an aircraft landing gear system has a hydraulic pressure source connected to a hydraulic fluid pressure transmission line, and at least one hydraulic
Vibration Control Of A Landing Gear System Featuring Electrorheological\\Magnetorheological Fluids Design For Civil Aircraft TFar-Field Drag-Prediction Technique Applied to Wing The feasibility and effectiveness of electrorheological (ER) and mag netorheological (MR) uid-based la... F Li,J Li,NM Were...