Examination of Fixed-Pitch Quadrotor Performance in a Slalom Maneuver Using Inverse Simulation
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-022-00516-w.pdf
Reference32 articles.
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4. Sun H, Lee S (2005) Response surface approach to aerodynamic optimization design of helicopter rotor blade. Int J Numer Meth Eng 64(1):125–142
5. Glaz B, Goel T, Liu L, Friedmann PP, Haftka RT (2009) Multiple-surrogate approach to helicopter rotor blade vibration reduction. AIAA J 47(1):271–282
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