Taylor, Brian2015-06-192015-06-192015-06-08https://hdl.handle.net/11299/172655The 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.enUMore Test RangeFenrir Flight 25Attitude and Airspeed HoldDoublet Phi and ThetaRigid Body Control Law SynthesisDataset