Taylor, Brian2015-06-192015-06-192015-06-08https://hdl.handle.net/11299/172654The 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. The pilot got too slow following launch and took a while to get to the test condition, so we only get a few seconds of data.enUMoreFenrirFlight 24Attitude and Airspeed HoldDoublet Phi and ThetaDataset