imu

IoT/AttitudeHeadingReferenceSystem-IMU.adoc

@@ -18,8 +18,7 @@ include::header.adoc[]
 
 An attitude and heading reference system (AHRS) consists of sensors on three axes that provide attitude information for aircraft, including roll, pitch and yaw. These are sometimes referred to as MARG (Magnetic, Angular Rate, and Gravity)[1] sensors and consist of either solid-state or microelectromechanical systems (MEMS) gyroscopes, accelerometers and magnetometers. They are designed to replace traditional mechanical gyroscopic flight instruments. 
 
-More Info: 
-https://en.wikipedia.org/wiki/Attitude_and_heading_reference_system[^]
+[More Info]https://en.wikipedia.org/wiki/Attitude_and_heading_reference_system[^]
 
 A basic IMU (Intertial Measurement Unit) generally provides raw sensor data, whereas an AHRS takes this data one step further, converting it into heading or direction in degrees, converting the raw altitude data into standard units like feet or meters, etc. 
 
@@ -29,7 +28,7 @@ A basic IMU (Intertial Measurement Unit) generally provides raw sensor data, whe
 
 image:./sensors_1604_LRG.jpg[alt="Adafruit 10-DOF IMU Breakout"]
 
-Adafruit's 10DOF (10 Degrees of Freedom)https://en.wikipedia.org/wiki/Degrees_of_freedom[^] breakout board allows you to capture ten distinct types of motion or orientation related data.
+Adafruit's 10DOF [(10 Degrees of Freedom)]https://en.wikipedia.org/wiki/Degrees_of_freedom[^] breakout board allows you to capture ten distinct types of motion or orientation related data.
 
 
 - LSM303DLHC - a 3-axis accelerometer (up to +/-16g) and a 3-axis magnetometer (up to +/-8.1 gauss) on a single die