High-Level Integration Sizing Tool for Electrical Architectures (HighLITE)
Author:
Affiliation:
1. PC Krause and Associates
2. Air Force Research Laboratory
Funder
Air Force Research Laboratory
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9813698/9813746/09813989.pdf?arnumber=9813989
Reference18 articles.
1. Performance Assessment of a Distributed Electric Propulsion System for a Medium Altitude Long Endurance Unmanned Aerial Vehicle
2. Feasibility assessments of a hybrid turboelectric medium altitude long endurance unmanned aerial vehicle;cinar;AIAA/IEEE 2020 Electric Aircraft Technology Symposium,2020
3. A Modelling Framework for Efficient Design of Electrical Power Systems for Electrical Propulsion Aircraft
4. Optimization of Electrical Energy Storage System Sizing for an Accurate Energy Management in an Aircraft
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