Results 21 to 30 of about 113,027 (258)

Design and Flight Performance of a Bio-Inspired Hover-Capable Flapping-Wing Micro Air Vehicle with Tail Wing

open access: yesAerospace, 2023
A key challenge in flapping-wing micro air vehicle (FWMAV) design is to generate high aerodynamic force/torque for improving the vehicle’s maneuverability. This paper presents a bio-inspired hover-capable flapping-wing micro air vehicle, named RoboFly.S,
Shengjie Xiao   +6 more
doaj   +1 more source

Performance of NIRCam on JWST in Flight

open access: yesPublications of the Astronomical Society of the Pacific, 2023
Abstract The Near Infrared Camera for the James Webb Space Telescope (JWST) is delivering the imagery that astronomers have hoped for ever since JWST was proposed back in the 1990s. In the Commissioning Period that extended from right after launch to early 2022 July, NIRCam has been subjected to a number of performance tests and ...
Rieke, Marcia J.   +54 more
openaire   +4 more sources

PARASOL in-flight calibration and performance [PDF]

open access: yesApplied Optics, 2007
Since 18 December 2004, the PARASOL satellite is a member of the so-called A-train atmospheric orbital observatory, flying together with Aqua, Aura, CALIPSO, CLOUDSAT, and OCO satellites. These satellites combine for the first time a full suite of instruments for observing aerosols and clouds, using passive radiometer complementarily with active lidar ...
Fougnie, B.   +5 more
openaire   +3 more sources

A Generalized Approach to Operational, Globally Optimal Aircraft Mission Performance Evaluation, with Application to Direct Lift Control

open access: yesAerospace, 2020
A unified approach to aircraft mission performance assessment is presented in this work. It provides a detailed and flexible formulation to simulate a complete commercial aviation mission.
Sam de Wringer   +2 more
doaj   +1 more source

In-Flight Performance of the LEKIDs of the OLIMPO Experiment [PDF]

open access: yesJournal of Low Temperature Physics, 2020
We describe the in-flight performance of the horn-coupled Lumped Element Kinetic Inductance Detector arrays of the balloon-borne OLIMPO experiment. These arrays have been designed to match the spectral bands of OLIMPO: 150, 250, 350, and 460 GHz, and they have been operated at 0.3 K and at an altitude of 37.8 km during the stratospheric flight of the ...
Paiella, A.   +24 more
openaire   +4 more sources

Three-Dimensional Flight Envelope for V/STOL Aircraft with Multiple Flight Modes

open access: yesAerospace, 2022
Vertical or short take-off and landing (V/STOL) aircraft generally have three flight modes, namely, vertical take-off and landing (VTOL), conversion, and cruise, according to the variable angle of propulsion direction to the fuselage axis.
Tielin Ma   +4 more
doaj   +1 more source

Improved Quality Management of the Indian Meal Moth, Plodia interpunctella (Hübner) (Lepidoptera: Pyralidae) for Enhanced Efficacy of the Sterile Insect Technique

open access: yesInsects, 2023
The sterile insect technique (SIT) is considered an environmentally friendly, autocidal control tactic to manage insect pests. This work dealt with the improvement of quality management of the Indian meal moth Plodia interpunctella (Hübner) for enhanced ...
Md. Mahbub Hasan   +2 more
doaj   +1 more source

Tri-Copter UAV With Individually Tilted Main Wings for Flight Maneuvers

open access: yesIEEE Access, 2020
A tri-copter unmanned aerial vehicle (UAV) with individually tilted main wings for various flight maneuvers is presented. In contrast to conventional tilt wing UAVs, thrust vectoring and control of the directions of main wing surfaces are attained by ...
Kyung-Jae Nam   +2 more
doaj   +1 more source

Determination of representative loading conditions for effective semitrailer design

open access: yesTransport, 2014
Obtaining a representative loading spectrum that corresponds well to the reality is still one of the greatest challenges for fatigue life calculations and optimal design of the trailer body.
Karel Kural   +3 more
doaj   +1 more source

Process Development for Integrated and Distributed Rotorcraft Design

open access: yesAerospace, 2019
The German Aerospace Center is currently developing a new design environment for rotorcraft, which combines sizing, simulation and evaluation tasks into one toolbox.
Peter Weiand   +2 more
doaj   +1 more source

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