Research on Landing Stability of Four-Legged Adaptive Landing Gear for Multirotor UAVs
Rotorcraft Unmanned Aerial Vehicles (UAVs) often need to take off and land under complex working conditions. The rugged terrains may cause the UAV to tilt during takeoff and landing and even cause rollover and other accidents in severe cases.
Xinlei Ni +4 more
doaj +2 more sources
A bifurcation study to guide the design of a landing gear with a combined uplock/downlock mechanism. [PDF]
This paper discusses the insights that a bifurcation analysis can provide when designing mechanisms. A model, in the form of a set of coupled steady-state equations, can be derived to describe the mechanism.
Knowles JA +3 more
europepmc +5 more sources
A Dynamic Pose-Testing Technique of Landing Gear Combined Stereo Vision and CAD Digital Model [PDF]
The landing gear is one of the key components of an aircraft, enduring significant forces during takeoff and landing, and is influenced by various uncertain factors related to its structure.
Wendong Zhang +3 more
doaj +2 more sources
A Mantis-Inspired Multi-Quadrupole Adaptive Landing Gear Design and Performance Study [PDF]
This paper investigates and designs an adaptive landing gear inspired by the passive adaptation mechanism of the praying mantis on intricate landing surfaces to improve the landing safety of unmanned aerial vehicles (UAVs) in complicated terrain ...
Yichen Chu +4 more
doaj +2 more sources
Modeling of dynamic responses of arresting gear and its sensitivity study based on BP neural network optimized by Whale optimization algorithm [PDF]
Arresting gear is the key equipment to ensure the safe and short-range landing of a carrier-based aircraft, which is a complex electromechanical-hydraulic system.
Qi Deng +5 more
doaj +2 more sources
Preliminary calculation of the landing gear of a military training aircraft [PDF]
The paper presents a preliminary calculation method, which is easy to apply for pre-dimensioning the landing gear. Preliminary calculation of the landing gear includes estimating the loads on landing and determining the position of the nose landing gear ...
Ilie NICOLIN, Bogdan Adrian NICOLIN
doaj +1 more source
Oleo-pneumatic Mixed Shock Absorber Landing Pressure Analysis of Landing Gear
The landing gear of an aircraft bears a large impact load during landing, which causes the internal shock absorber to withstand high oil pressure and air pressure, and the buffer performance is greatly influenced.
LOU Rui +3 more
doaj +1 more source
Research on the nose landing gear of a military training aircraft [PDF]
This paper presents the analysis of the landing gear configurations and the proposal of a solution for a military training aircraft. The paper presents both landing gears: nose and main because they are inextricably linked.
Ilie NICOLIN, Bogdan Adrian NICOLIN
doaj +1 more source
Optimization of the Main Landing Gear Structure of LSU-02NGLD
The mass of the landing gear structure becomes an important aspect of the total mass of the UAV (unmanned aerial vehicle). Therefore, many efforts have been made to reduce the mass of the landing gear by performing structural optimization.
Fajar Ari Wandono
doaj +1 more source
Influence of Cabin Doors on the Flow Field and Aerodynamic Noise of Landing Gear
The front landing gear generally has a bilateral symmetrical doors,which is different from the main landing gear.The opened landing gear door can interfere with the flow field and noise of the landing gear and reflect when the civil aircraft enters the ...
MU Yongfei, LI Jie
doaj +1 more source

