One day, looking for cheap sensors on ebay, I found this interesting board which contained everything I was looking for. It basically consists of a 3-axis accelerometer (ADXL345), a 3-axis magnetometer (HMC5883L), a 3-axis gyroscope (L3G4200D) and a barometric pressure sensor (BMP085). My plan is to build an Inertial Measurement Unit (IMU) (or maybe I should call it Attitude and heading reference system (AHRS)) and in the process learn how to interact and interpret the information all of this sensors provide. The fact is I have some experience using IMUs since I used one on my master thesis and another one on the Avora AUV, but the fact is they come preprogrammed and there is not much point in working with the raw sensor data unless you want to improve the measurement or give it another use.

For this project I am also using an Arduino Duemilanove, for that reason I wanted to call it ArduIMU, but there is already another project with the same name, so I will have to find another name (suggestions would be appreciated). Connecting the sensor board to the Arduino is pretty straightforward, every sensor has an *I²C* interface so you can access each of them using the Arduino Wire Library. The drawing was done using fritzing, on which I created the corresponding custom part for this board, although I did something wrong and it does not conform to the fritzing graphic standards.

This will be the first of a series of posts I plan to write about this project, since there are several steps I need to take in order to fully understand each sensor and several more to combine them in order to improve accuracy. In this post I want to talk about the accelerometer and how to obtain the roll and pitch angles from it, which is a process that can also be called tilt sensing.

Accelerometers are devices that are capable of measuring the acceleration they experience relative to free-fall, the same acceleration living beings feel. As a consequence, accelerometers are incapable of measuring the acceleration of gravity, but can be used to measure the upwards acceleration that counters gravity when at rest. This acceleration is measured as on the *z*-axis, when both pitch and roll angles are *zero*, but when the sensor is tilted either the *x*-axis or the *y*-axis experiences a component of the upward acceleration, whose magnitude depends on the tilt angle.

### Pitch & Roll estimation

Obtaining the pitch and roll angles is then a matter of being able to read the accelerometer, convert these readings to the *g* unit (*1g = 9.8 m/s²*), and apply the corresponding equations. The process of obtaining and converting the accelerometer readings depends on the accelerometer you are using, in my case, the ADXL345 in its basic configuration, provides 10-bit resolution for *±2g*, but has several other ranges (*±2g,* *±4g*, *±8g*, *±16g*) and resolutions (from 10 to 13 bits depending on the range) . Generalizing, the formula used to calculate the acceleration from the accelerometer readings is:

Once we have the correct acceleration components, we can proceed to calculate the different angles using the following equations:

For more information about where these equations come from, you can read the documentation I include at the end of this post. As you can see, the denominator of the pitch equation is defined to be always positive, so the equation itself only provides range, which is exactly what is expected for the pitch angle. In contrast, the roll equation provides range. It is important to take into account that when the pitch angle is *90º*, the surge axis (roll) is directly aligned with the gravity vector, thus we cannot measure the roll angle anymore, this is what is called Gimbal Lock.

Also, be aware that the roll equation is undefined when both and are equal to zero, and that for each possible value of the calculation done inside the *arctan* function there are two valid solutions, not only on the roll but also on the pitch equation. These problems can be easily solved in code by using the function *atan2*, which eliminates the angle calculation ambiguity by taking into account the quadrant.

### Removing short-term fluctuations using a Low-Pass filter

At this point we already have a fully functional pitch & roll estimation system, but if we experiment with it we will discover that the readings fluctuate quite a bit and this may be very annoying for some applications. Removing these short-term fluctuations can be achieved by means of what is called a Low-Pass filter. This type of filter attenuates the higher frequencies of the signal, thus providing a smoother reading. The Low-Pass filter is easily implemented by using the following equation:

Where is our filtered signal, the previous filtered signal, the accelerometer reading and the smoothing factor. It probably may seem obvious, but filtering should be done to the accelerometer readings before calculating the angles, instead of to the angles themselves. Regarding the smoothing factor, the lower we set it, the more it will take for the angle to stabilize, so we should not set it too low because then we could lose real-time behaviour. With this I mean that the reading will not correspond to the real angle until it stabilizes, and this could take some time.

### The source code & the ADXL345 library

I developed a small library to interface with the accelerometer, even though at the moment I have only implemented the basic functionality, I plan on supporting all of the device features. You can find it in my gitlab account. Thanks to the library, the code is pretty straightforward. It just reads the sensor accelerations which are already converted into *g*s by the library, applies the Low-Pass filter and then uses the roll and pitch equations to calculate the angles.

#include #include const float alpha = 0.5; double fXg = 0; double fYg = 0; double fZg = 0; ADXL345 acc; void setup() { acc.begin(); Serial.begin(9600); delay(100); } void loop() { double pitch, roll, Xg, Yg, Zg; acc.read(&Xg, &Yg, &Zg); //Low Pass Filter fXg = Xg * alpha + (fXg * (1.0 - alpha)); fYg = Yg * alpha + (fYg * (1.0 - alpha)); fZg = Zg * alpha + (fZg * (1.0 - alpha)); //Roll & Pitch Equations roll = (atan2(-fYg, fZg)*180.0)/M_PI; pitch = (atan2(fXg, sqrt(fYg*fYg + fZg*fZg))*180.0)/M_PI; Serial.print(pitch); Serial.print(":"); Serial.println(roll); delay(10); }

### Links & References

- Source | ADXL345-Accelerometer Arduino Library & Processing
- Documentation | AN3461 – Tilt Sensing Using Linear Accelerometers
- Fritzing Part | GY-80