Results 271 to 280 of about 416,562 (354)
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Rotorcraft Robotic Landing Gear with Locking Mechanisms
Journal of Dynamic Systems Measurement, and Control, 2023Robotic Landing Gear (RLG) for rotorcraft improves performance in landing on sloped uneven terrain, unprepared areas, and ship decks. The interaction between the feet of the RLG and the landing surface are pivotal to a successful landing event ...
Dooroo Kim, Cason Butler, M. Costello
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Aircraft Engineering and Aerospace Technology, 2022
Purpose The purpose of this paper is to control a landing gear system with an oleo-pneumatic shock absorber with the fuzzy controller. Design/methodology/approach The landing gear system with an oleo-pneumatic shock absorber is modeled mathematically.
Ahmet Enes Arık, B. Bilgiç
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Purpose The purpose of this paper is to control a landing gear system with an oleo-pneumatic shock absorber with the fuzzy controller. Design/methodology/approach The landing gear system with an oleo-pneumatic shock absorber is modeled mathematically.
Ahmet Enes Arık, B. Bilgiç
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Advanced landing gear fibre Bragg grating sensing and monitoring system
Advances in Structural Engineering, 2022In this paper an advanced optical-based landing gear load sensing and monitoring system is presented. The system measures strains using fibre Bragg grating sensor that are converted into loads and torque at the landing gear wheels and provides this data ...
F. Grooteman +5 more
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Analyses of Rear Landing Gear of a UAV Using Carbon Fibre Composites
ECS Transactions, 2022Nowadays unmanned aerial vehicles have become demanded in various sectors, such as military, health, photography, and weather monitoring. This paper is written to in order to choose a material for a landing gear.
Hardik S. Shukla +4 more
semanticscholar +1 more source
Aircraft Engineering and Aerospace Technology, 1974
DUNLOP LTD were selected to supply the tyres, wheels, and brakes, (hydraulic aspects are dealt with elsewhere). As in all cases of aircraft design, space, weight, performance and cost were of particular importance. The selection of suppliers for the MRCA was no exception when competing against many rivals and the division's experience and technology ...
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DUNLOP LTD were selected to supply the tyres, wheels, and brakes, (hydraulic aspects are dealt with elsewhere). As in all cases of aircraft design, space, weight, performance and cost were of particular importance. The selection of suppliers for the MRCA was no exception when competing against many rivals and the division's experience and technology ...
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2021
This chapter describes the results obtained during the TILDA Project on the additional LAGOON landing gear test case.
F. Chalot +4 more
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This chapter describes the results obtained during the TILDA Project on the additional LAGOON landing gear test case.
F. Chalot +4 more
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The Design of Aircraft Landing Gear
, 2021The aircraft landing gear and its associated systems represent a compelling design challenge: simultaneously a system, a structure, and a machine, it supports the aircraft on the ground, absorbs landing and braking energy, permits maneuvering, and ...
R. K. Schmidt
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Design, structure analysis and shock control of aircraft landing gear system with MR damper
Smart materials and structures (Print)This study proposes a new magneto-rheological aircraft main landing gear (MRAMLG) system and comprehensively treats from a mathematical modelling to drop testing for the evaluation of the landing efficiency.
Byung-Hyuk Kang, Seung-Bok Choi
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Aircraft Engineering and Aerospace Technology, 1975
IN deciding upon the precise form which the landing gear for the Hawk should take, Automotive Products, who were awarded the contract to provide the undercarriage, found it was necessary to consider a wide range of fundamental design requirements.
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IN deciding upon the precise form which the landing gear for the Hawk should take, Automotive Products, who were awarded the contract to provide the undercarriage, found it was necessary to consider a wide range of fundamental design requirements.
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Aircraft Engineering and Aerospace Technology, 1973
THE QUADRICYCLE CONFIGURATION landing gear chosen by the aircraft designers consists of a single wheel steerable nose leg, a twin wheel main leg, and two fully castoring single wheel outrigger legs at the wing tips. All retract aft into very confined spaces.
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THE QUADRICYCLE CONFIGURATION landing gear chosen by the aircraft designers consists of a single wheel steerable nose leg, a twin wheel main leg, and two fully castoring single wheel outrigger legs at the wing tips. All retract aft into very confined spaces.
openaire +1 more source