Implementation Implications of Hybrid-Electric Power Systems on Multi-Rotor UAS-Reference-Cited by-同舟云学术

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Implementation Implications of Hybrid-Electric Power Systems on Multi-Rotor UAS

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Information Systems-AIAA Infotech @ Aerospace
language:
Short-container-title:

Author:

McKinney Kristen¹,Feight Jordan A.¹,Gaeta Richard J.¹,Jacob Jamey D.¹

Affiliation:

1. Oklahoma State University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0986

Reference20 articles.

1. T. Hays, High Energy Density Propulsion Systems and Small Engine Dynamometer, M.S. thesis, Dept. Mech. Aero. Eng.,OklahomaState Univ., Stillwater, OK,2007.

2. Fuel Cells: A Real Option for Unmanned Aerial Vehicles Propulsion

3. Power and energy management system for fuel cell unmanned aerial vehicle

4. Development of a Dynamometer for Measuring Small Internal-Combustion Engine Performance

5. The control of a parallel hybrid-electric propulsion system for a small unmanned aerial vehicle using a CMAC neural network

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Validation of Analytical Model for Turboelectric Power System for Preliminary Design Purposes;Journal of Engineering for Gas Turbines and Power;2020-08-01

2. Detailed Analysis of the Implications of Implementing a Hybrid-Electric Power System on Multi-Rotor UAVs;2018 Aviation Technology, Integration, and Operations Conference;2018-06-24

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