Rapid Method for Computing Reachable Landing Distances in Helicopter Autorotative Descent



Eberle, Brian F, Rogers, Jonathan D, Alam, Mushfiqul and Jump, Michael ORCID: 0000-0002-1028-2334
(2022) Rapid Method for Computing Reachable Landing Distances in Helicopter Autorotative Descent. JOURNAL OF AEROSPACE INFORMATION SYSTEMS, 19 (7). pp. 504-510.

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Item Type: Article
Uncontrolled Keywords: Helicopters, Computing, Test Pilots, Banking Turn, Airspeed, Fixed Wing Aircraft, Avionics Systems, Graphics Processing Unit, Lift to Drag Ratio, Proportional Integral Derivative
Divisions: Faculty of Science and Engineering > School of Engineering
Depositing User: Symplectic Admin
Date Deposited: 16 Jun 2022 15:39
Last Modified: 18 Jan 2023 20:57
DOI: 10.2514/1.I011035
Related URLs:
URI: https://livrepository.liverpool.ac.uk/id/eprint/3156612