Fenrir Flight 26

Taylor, Brian
2015-06-10
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Fenrir Flight 26

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2015-06-10

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The goal for this flight was to run an updated attitude tracker to fix the deficiencies noticed in Flight 25. We mapped pilot sticks to provide a pitch and roll angle command (+/- 20 degrees from a 7 degree trim point in pitch and +/-35 degrees in roll). The pilot also had an auto throttle available to hold the aircraft at 23 m/s, which he engaged part way through the test run. The tracking looked very good and the pilot landed in the pitch / roll angle command mode.

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Taylor, Brian. (2015). Fenrir Flight 26. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172656.

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