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| author | Lorenz Meier <lm@inf.ethz.ch> | 2014-05-15 07:27:59 +0200 |
|---|---|---|
| committer | Lorenz Meier <lm@inf.ethz.ch> | 2014-05-15 07:27:59 +0200 |
| commit | 5f96feb3e0928be58b96d5adbebc33e14ea2a690 (patch) | |
| tree | 8fe73f6aa60645b16b36bc6ff0b6c747e5e31fc3 /src/modules/mc_att_control/mc_att_control_main.cpp | |
| parent | 23fe9e6dc0cfa77eac0af1a789a22b2e56bdb84e (diff) | |
| download | px4-firmware-5f96feb3e0928be58b96d5adbebc33e14ea2a690.tar.gz px4-firmware-5f96feb3e0928be58b96d5adbebc33e14ea2a690.tar.bz2 px4-firmware-5f96feb3e0928be58b96d5adbebc33e14ea2a690.zip | |
mc_att_control: Code style fixes in comments
Diffstat (limited to 'src/modules/mc_att_control/mc_att_control_main.cpp')
| -rw-r--r-- | src/modules/mc_att_control/mc_att_control_main.cpp | 9 |
1 files changed, 5 insertions, 4 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 a69153bf0..74e31dd5b 100644 --- a/src/modules/mc_att_control/mc_att_control_main.cpp +++ b/src/modules/mc_att_control/mc_att_control_main.cpp @@ -1,9 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. - * Author: @author Tobias Naegeli <naegelit@student.ethz.ch> - * @author Lorenz Meier <lm@inf.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,9 +32,13 @@ ****************************************************************************/ /** - * @file mc_att_control_main.c + * @file mc_att_control_main.cpp * Multicopter attitude controller. * + * @author Tobias Naegeli <naegelit@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> + * * 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. * For small deviations controller rotates copter to have shortest path of thrust vector and independently rotates around yaw, |