Description
The goal for this flight was to put doublets on theta and then phi commands to test attitude tracking. An auto throttle was running with a set point of 23 m/s during the doublets. We got a full pitch doublet and observed good pitch tracking, but poor roll tracking.
Suggested Citation
Taylor, Brian.
(2015).
Fenrir Flight 25.
Retrieved from the University of Minnesota Digital Conservancy,
https://hdl.handle.net/11299/172655.