Thor Flight 25

2011-10-05

Title

Thor Flight 25

Published Date

2011-10-05

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Abstract

Description

The 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.

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Suggested citation

Taylor, Brian. (2011). Thor Flight 25. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/174304.

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