AeroQuad is an open-source hardware and software project dedicated to the construction of remote controlled four-rotor helicopters, also known as quadcopters or quadrocopters.AeroQuad hardware typically consists of an Arduino microcontroller (Mega-2560 or Uno) as the flight controller board, and an AeroQuad shield with various sensors, such as an accelerometer and gyroscope.
AeroQuad software, written mostly in C and uploaded to the micro-controller via the Arduino IDE, currently supports Rate (Acrobatic) Mode that uses only the gyroscope for flight assistance, and Attitude (Stable) Mode that use both the gyroscope and accelerometer for auto-leveled flight assist.
There are also additional sensors that provide a number of other optional functions, such as heading or altitude hold.

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The AeroQuad flight control board supports the standard quartet of motors (front, mid, rear and tail) and multiple flight modes (rate, attitude and altitude hold). By default the AeroQuad flight control board is always in Attitude (stable) Mode and the flight controller holds position by using the throttle to maintain pitch and roll at zero degrees. The flight controller takes the role of the previously separate accelerometer and gyroscope while maintaining a synchronized state, allowing for easier use of either sensor individually for roll and pitch, instead of both. In Attitude (stable) mode the flight controller uses the gyroscope for attitude, and the accelerometer as reference for rate correction. In Rate (acrobatic) mode the flight controller uses the accelerometer to measure rate to correct rate rather than attempting to hold a set rate and simultaneously hold roll and pitch at zero degrees. In all other modes the accelerometer and gyroscope are used for rates corrections and reference for roll and pitch.
AeroQuad Components:
Flight Controller Module:
ArduCAM aeroquad:
ArduQuad aeroquad:
AeroQuad Flight Controller:
ArduPilotAeroQuad Arduino Core Library:
ArduPilot Mega Barebones:
Demo Videos
Full Duplex With Accelerometer
Demo Video With Acc and Gyro
Photo Gallery
References
Category:Unmanned aerial vehicles of the United States (K+), pH 7.4. The level of luminescence was determined using the IVIS Imaging System (Perkin Elmer, Waltham, MA). Images were captured using Living Image software and analyzed with Living Image software.
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AeroQuad 3.0.1 Free
The core AeroQuad platform (microcontroller + operating system + programing) is licensed under the GNU GPL v3.
The AeroQuad platform itself (shield, connectors etc.) is licensed under the GNU LGPL v2.1.
AeroQuad currently supports Arduino Boards (Mega and Uno) and Pixhawk (Quad) devices.
AeroQuad is compatible with the following sensors:
Steering (Heading/Vertical Position)
Altitude hold
GPS
Gyroscope
Compass
Accelerometer
And there are a number of available motor configurations:
4 motor Quadcopter /
2 motor Cycloid /
1 motor Cycloid /
1 motor Cycloid /
Single Motor Cycloid /
Single Motor Cycloid /
Each of the different motors can be controlled with:
Aeropower
LMK 1.1/2.0/2.1
Pixhawk (MPU6050/9152)
(Steer 2.0)
AeroQuad Intro:
AeroQuad is based on two main components, the accelerometer (gyro) and the
steering (heading) signal.
The landing/take off behavior is based on the angle/angle rate input.
The landing/take off behavior of the crash landing is based on time elapsed
from the crash.
The crash landing performance is based on reference system.
AeroQuad Certification:
The behavior of AeroQuad is based on the data acquired from the sensors,
which are plugged into the microcontroller via the Arduino board.
Therefore the performance of the behavior is certified by the
Data Acquired Signal (DAS) of the Arduino board.
The behavior of the crashed landing is based on the angle and angle rate
inputs.
The crash landing behavior is also certified with the angle and angle
rate input.
Performance of the crash landing behavior is based on the reference system.
AeroQuad Specifications:
Microcontroller: Arduino
Stabilization: Aeropower
Number of motors:
Position Hold:
What’s New in the AeroQuad?
AeroQuad is an open-source hardware and software project dedicated to the construction of remote controlled four-rotor helicopters, also known as quadcopters or quadrocopters.
This article will focus on the design and construction of the Stable Mode flight control software for the AeroQuad.
The hardware overview and main specifications are outlined below.
Hardware Overview:
The hardware consists of an Arduino microcontroller (Mega-2560 or Uno) as the flight controller board, and an AeroQuad shield with various sensors, such as an accelerometer and gyroscope. The microcontroller interfaces with the various sensors using a system known as “I2C”, or “Inter-IC”, which is an industry standard protocol that allows one device, such as the Arduino, to talk to another device, such as a sensor.
The sensor can be one of many different types, but the Arduino usually only has a very basic analog input. By using an I2C sensor to monitor an analog voltage input, the Arduino is able to detect when a set voltage is exceeded or not exceeded. The Arduino also has a UART (Universal Asynchronous Receiver/Transmitter) that allows the Arduino to talk to the computer or PC through a serial connection.
The shield contains a number of connectors that can be used to connect various sensors or actuators that a user can purchase. The Aerowire shield uses the standard Arduino power adapter (5V, regulated down to 3.3V) and includes the power connector for the digital and the analog input, the servo connector, and a number of high-speed digital and analog pins.
The Arduino software uses the standard Arduino IDE that allows the user to view the wiring diagram of an Arduino project and upload the code. This also allows the user to access the system information such as the version of the software and serial port settings.
Software Overview:
The software typically consists of two parts. First, there is a dynamic flight controller that uses I2C to communicate with the various sensors to detect motion. The idea is that the sensors and other inputs provide information to the flight controller so it can steer the quad and avoid obstacles. Second, a static flight assist algorithm will be used to allow the quad to automatically control and stabilize the plane.
A number of examples of code using I2C have
System Requirements For AeroQuad:
Supported OS: Windows 10 (64-bit, Windows 7/8/8.1 (32-bit only), Windows Server 2008/2012/2016 (64-bit only), Linux. Note: Mac OS users are not supported.
Processor: Intel i3, Intel i5, Intel i7 (models that support Hyper-threading are preferred)
Memory: 2 GB or more RAM
Video Card: Nvidia GTX 770 or better, AMD Radeon HD7870 or better
DirectX: Version 11
Networking: Broadband Internet connection
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