Skoll Flight 3

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skoll_flight03_2015_07_02.mat (17.97 MB)
skoll_flight03_analysis.m (1.58 KB)
Skoll Flight 3 Report.pdf (214.83 KB)
Skoll_Flight03_2015_07_02_3211_Pitch_Surfaces.mp4 (52.15 MB)
Skoll_Flight03_2015_07_02_3211_Roll_Surfaces.mp4 (37.81 MB)
Winglet Art v2 - Left.png (44.32 KB)
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/11299/172735

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Journal Title

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Title

Skoll Flight 3

Authors

Taylor, Brian

Published Date

2015-07-02

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Abstract

Keywords

Skoll Flight 3

UMore Test Range

Rigid Body Aerodynamics

Control Law Performance

Stall Speed

Climb Rate

Description

The goal for this flight was to conduct three tests during the available straight leg passes at 20 m/s: 1. to conduct 3-2-1-1 excitations on pitch surfaces, 2. to conduct 3-2-1-1 excitations on roll surfaces, and 3. to test a theta ref doublet with a higher gain control law to evaluate performance of the higher gains. All of these tests were completed successfully with 8 pitch excitations, 8 roll excitations, and the theta doublet.

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Suggested citation

Taylor, Brian. (2015). Skoll Flight 3. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172735.

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