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301
Ground Motion Modeling and Adaptive Joint Control for Large-Scale UAVs
Published 2024-12-01Get full text
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302
Numerical Simulations of the Impact and Spreading of a Particulate Drop on a Solid Substrate
Published 2012-01-01Get full text
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303
Fault Tree Interval Analysis of Complex Systems Based on Universal Grey Operation
Published 2019-01-01“…Next, the reliability of the aircraft landing gear retraction system is evaluated despite insufficient statistical information describing failures. …”
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304
Autonomous Close Formation Flight Control with Fixed Wing and Quadrotor Test Beds
Published 2016-01-01“…This paper discusses the implementation and flight testing of nonlinear dynamic inversion (NLDI) controllers for close formation flight (CFF) using two distinct UAV platforms: a set of fixed wing aircraft named “Phastball” and a set of quadrotors named “NEO.” …”
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305
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306
Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
Published 2021-01-01“…The proposed method is based on DEA, with QAR information as the analysis data, and four factors including engine working state, fuel/oil working state, aircraft flight state, and external conditions are considered to analyse the rotor vibration reliability. …”
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307
Algorithm for preliminary processing of charge coupled devices array data based on the adaptive Wiener filter
Published 2021-03-01“…When registering a signal from aircraft which provide maximum coverage of the studied area, it is important to obtain a signal with the maximum signal-to- noise ratio in a minimum time, since the accumulation of spectra samples for averaging is impossible. …”
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308
Optimal design and operation of a wind farm/battery energy storage considering demand side management
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309
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310
Autonomous Emergency Gliding Landing Guidance and Control of Tilt-Wing Electric Vertical Take-Off and Landing for Urban Air Mobility Missions Using Control Barrier Functions
Published 2025-01-01“…Urban Air Mobility (UAM) aims to transform urban transportation through innovative applications of electric Vertical Take-Off and Landing (eVTOL) aircraft. This paper focuses on tilt-wing eVTOLs, which offer significant advantages in energy efficiency and operational versatility. …”
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311
Requirements of Aerial Applicators in Florida
Published 2005-09-01“… This guide explains the requirements for applying pesticides, fertilizer and seed with an aircraft in Florida. This document is PI-58, one of a series of the Pesticide Information Office, Florida Cooperative Extension Service, Institute of Food and Agricultural Sciences, University of Florida. …”
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312
No more flying blind: Leveraging weather forecasting for clear-cut risk-based decisions
Published 2025-03-01“…Unmanned aircraft systems (UASs) have experienced a notable surge in applications, particularly with the increasing deployment of vertical take-off and landing (VTOL) vehicles in urban environments, which are more flexible in comparison to traditional aircraft. …”
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313
Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors
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314
UAV Detect and Avoid from UTM-Dependent Surveillance
Published 2024-01-01“…A hierarchical unmanned aircraft system (UAS) traffic management (UTM) system has deployed 45 ground transceiver stations (GTS) for UAS services in Taiwan. …”
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315
Control system for noise-resistant electronic speed controller of a brushless electric motor for an unmanned aerial vehicle
Published 2024-02-01“…The high demand for unmanned aircraft and their efficiency makes the production of their components a matter of relevance. …”
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316
Effect of Boron Carbide Particles Addition on the Mechanical and Wear Behavior of Aluminium Alloy Composites
Published 2023-01-01“…These prepared composites can be used for wing root fitting of an aircraft.…”
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317
Fatigue Life Analysis of Aluminum Alloy Notched Specimens under Non-Gaussian Excitation based on Fatigue Damage Spectrum
Published 2021-01-01“…In this study, a non-Gaussian excitation acceleration method is proposed, using aluminum alloy notched specimens as a research object and measured acceleration signal of a certain airborne bracket, during aircraft flight as input excitations, based on the fatigue damage spectrum (FDS) theory. …”
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318
Safety Assessment and Risk Estimation for Unmanned Aerial Vehicles Operating in National Airspace System
Published 2018-01-01“…When midair collision fatality risk is estimated, a model of aircraft collisions based on the density of civil flight in different regions over Chinese airspace is proposed. …”
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319
Requirements of Aerial Applicators in Florida
Published 2005-09-01“… This guide explains the requirements for applying pesticides, fertilizer and seed with an aircraft in Florida. This document is PI-58, one of a series of the Pesticide Information Office, Florida Cooperative Extension Service, Institute of Food and Agricultural Sciences, University of Florida. …”
Get full text
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320