From dc28c475443f40e9b0508d13dc1ef59abf16f811 Mon Sep 17 00:00:00 2001 From: Matthias Grob Date: Sat, 3 Mar 2018 20:57:32 +0000 Subject: [PATCH] mc_att_control: correct head comment --- src/modules/mc_att_control/mc_att_control_main.cpp | 5 +++-- 1 file changed, 3 insertions(+), 2 deletions(-) diff --git a/src/modules/mc_att_control/mc_att_control_main.cpp b/src/modules/mc_att_control/mc_att_control_main.cpp index 07a78a56c8..9cb2503dd9 100644 --- a/src/modules/mc_att_control/mc_att_control_main.cpp +++ b/src/modules/mc_att_control/mc_att_control_main.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013-2017 PX4 Development Team. All rights reserved. + * Copyright (c) 2013-2018 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -37,12 +37,13 @@ * * Publication documenting this type of Quaternion Attitude Control: * Nonlinear Quadrocopter Attitude Control (2013) - * by Dario Brescianini, Markus Hehn and Raffaello D’Andrea + * by Dario Brescianini, Markus Hehn and Raffaello D'Andrea * Institute for Dynamic Systems and Control (IDSC), ETH Zurich * * @author Lorenz Meier * @author Anton Babushkin * @author Sander Smeets + * @author Matthias Grob * * The controller has two loops: P loop for angular error and PD loop for angular rate error. * Desired rotation calculated keeping in mind that yaw response is normally slower than roll/pitch.