From 5f96feb3e0928be58b96d5adbebc33e14ea2a690 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Thu, 15 May 2014 07:27:59 +0200 Subject: mc_att_control: Code style fixes in comments --- src/modules/mc_att_control/mc_att_control_main.cpp | 9 +++++---- 1 file changed, 5 insertions(+), 4 deletions(-) (limited to 'src/modules/mc_att_control/mc_att_control_main.cpp') 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 - * @author Lorenz Meier - * @author Anton Babushkin * * 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 + * @author Lorenz Meier + * @author Anton Babushkin + * * 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, -- cgit v1.2.3