The ability of UAV’s (Unmanned Aerial Vehicles) to land on unknown and uneven terrain is an important area of research, particularly for applications such as field surveillance. This paper presents a novel solution to this problem using mechanical design, with a legged landing gear design that provides both suspension and stability on uneven terrain. The key features of this design are differen...

A hybrid approach is used to investigate the noise generated by a simplified landing gear without small scale parts such as hydraulic lines and fasteners. The Ffowcs Williams and Hawkings equation is used to predict the noise at far-field observer locations from flow data provided by an unsteady computational fluid dynamics calculation. A simulation with 13 million grid points has been complete...

A tire and landing gear test facility has been developed and incorporated into a Convair 990 aircraft. The system can simulate tire vertical load profiles to 250,000 lb, sideslip angles to 15 degrees, and wheel braking on actual runways. Onboard computers control the preprogrammed test profiles through a feedback loop and also record three axis loads, tire slip angle, and tire condition. The ai...

The landing gear of an aircraft serves to mitigate the vibration and impact forces transmitted from ground fuselage. This paper addresses magneto-rheological (MR) damper gear, which provides high shock absorption efficiency excellent stability in various conditions by adjusting damping force using external magnetic field intensity. performance MR was verified through numerical simulations drop ...

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 Dassault Aviation. The property to be verified states that the gear must be down in at most 14 seconds. ...