From a7d7c69a79f1ddb7ffbaa299fed41aa0a9a6a1a2 Mon Sep 17 00:00:00 2001
From: Daniel Agar <daniel@agar.ca>
Date: Sun, 7 Jun 2015 21:37:07 -0400
Subject: [PATCH] fix mixers README.md

-the angle brackets in the tag descriptions were breaking the markdown
---
 ROMFS/px4fmu_common/mixers/README.md | 24 ++++++++++++------------
 1 file changed, 12 insertions(+), 12 deletions(-)

diff --git a/ROMFS/px4fmu_common/mixers/README.md b/ROMFS/px4fmu_common/mixers/README.md
index b766d05aac..0e591ca288 100644
--- a/ROMFS/px4fmu_common/mixers/README.md
+++ b/ROMFS/px4fmu_common/mixers/README.md
@@ -34,7 +34,7 @@ collection of mixers in order to achieve a specific pattern of actuator outputs.
 
 The null mixer definition has the form:
 
-  Z:
+	Z:
 
 #### Simple Mixer ####
 
@@ -44,8 +44,8 @@ applying an output scaler.
 
 A simple mixer definition begins with:
 
-  M: <control count>
-  O: <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
+	M: <control count>
+	O: <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
 
 If <control count> is zero, the sum is effectively zero and the mixer will
 output a fixed value that is <offset> constrained by <lower limit> and <upper
@@ -59,7 +59,7 @@ offset of -0.5 is encoded as -5000.
 The definition continues with <control count> entries describing the control
 inputs and their scaling, in the form:
 
-  S: <group> <index> <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
+	S: <group> <index> <-ve scale> <+ve scale> <offset> <lower limit> <upper limit>
 
 The <group> value identifies the control group from which the scaler will read,
 and the <index> value an offset within that group.  These values are specific to
@@ -81,16 +81,16 @@ into a set of actuator outputs intended to drive motor speed controllers.
 
 The mixer definition is a single line of the form:
 
-R: <geometry> <roll scale> <pitch scale> <yaw scale> <deadband>
+	R: <geometry> <roll scale> <pitch scale> <yaw scale> <deadband>
 
 The supported geometries include:
 
-  4x - quadrotor in X configuration
-  4+ - quadrotor in + configuration
-  6x - hexcopter in X configuration
-  6+ - hexcopter in + configuration
-  8x - octocopter in X configuration
-  8+ - octocopter in + configuration
+ * 4x - quadrotor in X configuration
+ * 4+ - quadrotor in + configuration
+ * 6x - hexcopter in X configuration
+ * 6+ - hexcopter in + configuration
+ * 8x - octocopter in X configuration
+ * 8+ - octocopter in + configuration
   
 Each of the roll, pitch and yaw scale values determine scaling of the roll,
 pitch and yaw controls relative to the thrust control.  Whilst the calculations
@@ -102,4 +102,4 @@ thrust input ranges from 0.0 to 1.0.  Output for each actuator is in the
 range -1.0 to 1.0.
 
 In the case where an actuator saturates, all actuator values are rescaled so that 
-the saturating actuator is limited to 1.0.
\ No newline at end of file
+the saturating actuator is limited to 1.0.