Skoll Flight 4

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skoll_flight04_2015_07_09.mat (14.38 MB)
skoll_flight04_analysis.m (1.87 KB)
Skoll Flight 4 Flight Report.pdf (821.48 KB)
Winglet Art v2 - Left.png (44.32 KB)
Skoll_Flight04_2015_07_09_3211_Pitch_Surface.mp4 (34.86 MB)
Skoll_Flight04_2015_07_09_3211_Roll_Surface.mp4 (31.57 MB)
mAEWing1 Camera Location.PDF (66.55 KB)
mAEwing1 Camera Calibration Technique.pdf (92.29 KB)
cameraParameters class.pdf (349.78 KB)
CameraParameters.mat (3.39 KB)
FrameRIPPER.m (1.03 KB)
UndistortVideo.m (2.1 KB)

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https://hdl.handle.net/11299/172917

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Title

Skoll Flight 4

Authors

Taylor, Brian

Published Date

2015-07-09

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Abstract

Keywords

Skoll Flight 4

UMore Test Range

Rigid Body Aerodynamics

Flexible Body Dynamics

Description

The goal for this flight was to conduct two tests during the available straight leg passes at 30 m/s: 1. to conduct 3-2-1-1 excitations on pitch surfaces and 2. to conduct 3-2-1-1 excitations on roll surfaces. Both of these tests were completed successfully with 6 pitch excitations and 6 roll excitations. Pitch oscillations were observed during the tests suggesting interaction with flexible body dynamics.

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Suggested citation

Taylor, Brian. (2015). Skoll Flight 4. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172917.

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