The Quanser AERO is a fully integrated dual-motor lab experiment, designed for advanced control research and aerospace applications, that can also be used for teaching control concepts at the undergraduate level.
Features
Courseware
System Configuration
Specifications
Features
Compact and integrated system
High-efficiency coreless DC motors
High resolution optical encoder
Pitch & yaw axes and DC motors/rotors speed measurements through digital tachometer
Built-in voltage amplifier with integrated current sensor
Integrated data acquisition (DAQ) device
Flexible QFLEX 2 computing interface for USB and SPI connections
User-controllable tri-color LED
Easy-connect cables and connectors
Open architecture design, allowing users to design their own controller
Fully compatible with MATLAB®/Simulink® and LabVIEW™
Fully documented system models and parameters provided for MATLAB®/Simulink®, LabVIEW™
ABET-aligned, modular, digital media courseware provided for the Quanser AERO USB
Microcontroller examples and interfacing datasheet provided for the Quanser AERO Embedded
Courseware
ABET-aligned Instructor and Student Workbooks with complete lab exercises, covering topics
Hardware integration
Single propeller speed control
1 DOF attitude control configuration
PID control
Introduction to IMU
Modeling and model validation using transfer function
System identification
Gain scheduling
Laboratory Guides with modeling and control design examples
2 DOF helicopter configuration
Modeling
Linear state-space representation
State-feedback control
Coupled dynamics
Half-quadrotor configuration
Modeling
Simple yaw control
Kalman filter
System Configuration
The following additional components are required to complete your workstation, and are sold separately:
For USB QFLEX Panel
QUARC® add-on for MATLAB®/Simulink®
For NI myRIO QFLEX Panel
NI myRIO embedded device
For Embedded QFLEX Panel
Microprocessor (e.g. Arduino, Raspberry Pi)
Specifications
Base dimensions (W x D x H)
17.8 cm x 17.8 cm x 7 cm
Device height
35.6 cm (with propeller in horizontal position)
Device length
51 cm
Device mass
3.6 kg
Propeller diameter
12.7 cm
Yaw angle range
360º
Elevation angle range
124º (± 62º from horizontal) half-quadrotor configuration