Taylor, Brian2015-09-082015-09-082011-10-05https://hdl.handle.net/11299/174304The controller used for flight 23 was the baseline controller. For 24 and 25 it was the composite student controller, with the following gains: pitch_gain[3] ={-0.6, -0.09, 0.08}; group 1, v1 roll_gain[3]={-0.45, -0.022, 0.05}; group 3, v1 Software used was /branches/flightcode_nav/ rev 643 for flight 23, rev 645 for flights 24 and 25. Thor Flight 25: student controller, system id multisine input on the rudder. Straight and level for 3 seconds, then hold elevator and inject a 15 second multisine that covers 0.2 to 3.0 Hz, amplitude 3 deg. Lateral-directional controller still engaged. Onboard video and motor data collected. R/C Rx: A=21,L=0,F=0,H=0.en-USThor FlightACRCAnokaControlSystem IdentificationMultisineDataset