Taylor, Brian2015-07-022015-07-022015-07-02https://hdl.handle.net/11299/172735The goal for this flight was to conduct three tests during the available straight leg passes at 20 m/s: 1. to conduct 3-2-1-1 excitations on pitch surfaces, 2. to conduct 3-2-1-1 excitations on roll surfaces, and 3. to test a theta ref doublet with a higher gain control law to evaluate performance of the higher gains. All of these tests were completed successfully with 8 pitch excitations, 8 roll excitations, and the theta doublet.enSkoll Flight 3UMore Test RangeRigid Body AerodynamicsControl Law PerformanceStall SpeedClimb RateDataset