Thor Flight 20

Taylor, Brian
2011-07-26
Thumbnail Image

View/Download File

Thor Flight 20_Flight Report.pdf (128.28 KB)
thor_flight20_olpyr_doublet_2011_07_26.h5 (19.8 MB)
thor_flight20_olpyr_doublet_2011_07_26.mat (2.48 MB)

Persistent link to this item

https://hdl.handle.net/11299/174298
Statistics
View Statistics

Journal Title

Journal ISSN

Volume Title

Title

Thor Flight 20

Authors

Published Date

2011-07-26

Publisher

Type

Dataset

Abstract

Keywords

Description

Thor Flight 20: Open loop pitch-yaw-roll doublet. Wings level for 4 sec; then open loop (hold controller commands). 3 degree elevator doublet at 5 sec (1 sec period), 1.5 degree rudder doublet at 8 sec (1.5 sec period), 4 degree roll doublet at 12 sec (1 sec period).Purpose for this test was to compare the doublet response of the alpha-beta sensor to the simulation. The aircraft did not hold wings level very well due to the turbulence. Multiple repeats were done, and a few runs were completed successfully. R/C Rx: A=2,L=2,F=0,H=0.

Related to

Replaces

License

Collections

Flight Data

Series/Report Number

Funding information

Isbn identifier

Doi identifier

Previously Published Citation

Other identifiers

Suggested citation

Taylor, Brian. (2011). Thor Flight 20. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/174298.

Content distributed via the University Digital Conservancy may be subject to additional license and use restrictions applied by the depositor. By using these files, users agree to the Terms of Use. Materials in the UDC may contain content that is disturbing and/or harmful. For more information, please see our statement on harmful content in digital repositories.