VFS-F59-000275: Opposed Lateral Tilting (OLT) For Hover Pitch Control: A Preliminary Analysis of Aircraft Stability, Control Loads, and Scalability - Technical Paper

Event: Forum 59 - Phoenix, AZ 2003

Authors

gress aerospace

Abstract

Content: Opposed Lateral Tilting (OLT) For Hover Pitch Control: A Preliminary Analysis of Aircraft Stability, Control Loads, and Scalability - A Presentation

Meta Tags

Topics: Aircraft
Pitch

Affiliated or Co-Author: gress aerospace

Details

DOI: https://doi.org/10.4050/VFS-F59-000275

Citation: Gress, G., "Opposed Lateral Tilting (OLT) For Hover Pitch Control: A Preliminary Analysis of Aircraft Stability, Control Loads, and Scalability," Forum 59 - Phoenix, AZ 2003, Phoenix, AZ, May 6, 2003, https://doi.org/10.4050/VFS-F59-000275.

Additional Details

Publisher: The Vertical Flight Society

Published: 5/6/2003

Product Code: VFS-F59-000275

Content Type: Technical Paper

Language: English