Results 31 to 40 of about 2,944,878 (288)
Experimental assessment of low noise landing gear component design [PDF]
Landing gear related airframe noise is one of the dominant aircraft noise components atapproach, so continued research efforts to reduce landing gear noise are essential.
Chow, Leung Choi +13 more
core +1 more source
SIMULATION EXPERIMENT ON LANDING SITE SELECTION USING A SIMPLE GEOMETRIC APPROACH [PDF]
Safe landing is an important part of the planetary exploration mission. Even fine scale terrain hazards (such as rocks, small craters, steep slopes, which would not be accurately detected from orbital reconnaissance) could also pose a serious risk on ...
W. Zhao +9 more
doaj +1 more source
Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System [PDF]
Under certain conditions during takeoff and landing, pilots may sometimes experience vibrations in the cockpit. Because the cockpit is located right above the nose landing gear, which is known to potentially be prone to self-excited vibrations at certain
Lowenberg, Mark H +3 more
core +1 more source
Bifurcation analysis of nose landing gear shimmy with lateral and longitudinal bending [PDF]
We develop and study a model of an aircraft nose landing gear with torsional, lateral and longitudinal degrees of freedom. The corresponding three modes are coupled in a nonlinear fashion via the geometry of the landing gear in the presence of a nonzero ...
Thota, P +5 more
core +1 more source
Plasma Sheath around Chandrayaan-3 Landing Site: A Case Study
India’s lander-rover mission Chandrayaan-3 is scheduled to be launched in mid-2023. We have simulated a realistic scenario and investigated the electric potential development over the Chandrayaan-3 landing site under the influence of observed solar ...
Trinesh Sana, S. K. Mishra
doaj +1 more source
Thermal Modeling of the Lunar Regolith at the Chang'E‐4 Landing Site
Accurate assessments of surface temperatures on the Moon are important for understanding the physical properties of the lunar surface regolith and thermal effects on the reflectance spectra beyond 2 μm.
Honglei Lin +11 more
doaj +1 more source
On 14 December 2013 (UTC), China’s Chang’E-3 (CE-3) succeeded in landing on the Moon’s surface. The CE-3 landing site is in northern Mare Imbrium and several tens of meters away from the rim of a young crater with a few hundred meters in diameter.
Man-Hei Ng +3 more
doaj +1 more source
UAV Positioning Mechanisms in Landing Stations: Classification and Engineering Design Review
Landing platforms’ automation is aimed at servicing vertical take-off and landing UAVs between flights and maintaining their airworthiness. Over the last few years, different designs for the landing platforms have been proposed.
Musa Galimov +2 more
doaj +1 more source
SUITABLE LANDING SITE SELECTION FOR UNMANNED AERIAL VEHICLES USING AIRBORNE LASER SCANNING POINT CLOUD [PDF]
In the context of autonomous landing for unmanned aerial vehicles (UAVs), selecting a suitable landing site is crucial. This research presents a new method for automatically identifying safe landing sites based on point cloud data acquired through an ...
D. P. Singh, M. Yadav
doaj +1 more source
Observation-based temperature field simulation at Zhurong landing site, Mars
Modeling the temperature field near the Martian surface is critical for many scientific exploration tasks, such as detecting liquid water and analyzing the existence of saline ice.
Lei Zhang +7 more
doaj +1 more source

