The 2 DOF (Degrees of Freedom) Helicopter offers the student a unique opportunity to control the pitch and yaw of a simplified Helicopter model.
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2 DOF Helicopter
1. With Quanser the possibilities are infinite + 1 ( 9 0 5 ) 9 4 0 - 3 5 7 5 w w w . q u a n s e r. c o m
Description
Key Features Curriculum Topics
• Disturbance Rejection
• Tracking Control & Regulation
• Coupled Systems
• Full State-Feedback
• Observer Design & Implementation
• Frequency Analysis
• System Modeling & Simulation
• Pole-Placement Technique
• Root Locus Design
• Non-Linear Friction
• Hardware in the Loop
• Real-Time Control
• Discrete Time Sampling
• System Identification
• Multivariable Control Design
Product Information Sheet S2 - 1 - rev. C
Quanser has developed an extensive range of complex Specialty Challenges, a select sample
of these experiments includes:
The 2 DOF Helicopter is an Aerospace Control Challenge, and part of the Quanser Specialty
Control Challenge Range. Other Aerospace Control Challenges include:
For details of these experiments and more, visit our website www.quanser.com
Range of Quanser
Specialty
Experiments
Related Aerospace
Challenges
Specialty Control Challenges
MAGLEV – Magnetic Levitation
Shaker Tables and Smart Structures
2 DOF Serial Flexible Link / Joint
Heatflow Experiment
Coupled Tanks
Industrial Mechatronic Drives Unit
High Fidelity Linear Cart System
Triple Inverted Pendulum, Dual Inverted Pendulum ….
5 DOF Open Architecture Robots
Mechatronics Kit
The Cube
3 DOF Crane
Aerospace Control Challenges
• 3 DOF Helicopter • 3 DOF Hover
• Fully compatible with Matlab/Simulink & LabVIEW
• Open architecture design
• High Quality Slipring allows for unlimited yaw
• High Resolution Encoders to sense position and
rate feedback of yaw and pitch axis
• High Quality Aluminum chassis with precision
crafted parts
• Equipped with safety grills surrounding both
propeller blades to eliminate injury
• Fully documented system models & parameters
The 2 DOF (Degrees of Freedom) Helicopter offers the student a
unique opportunity to control the pitch and yaw of a simplified
Helicopter model. Actuated by 2 DC motors, mounted at 90 degrees
to each other, it has the ability to pitch and yaw. The Helicopter
frame is free to rotate on a vertical base equipped with an electrical
contact slipring. Electrical signals to and from the Helicopter are
channeled through the slipring to eliminate tangled wires, reduce
friction and allow for unlimited and unhindered yaw. The coupling
between the pitch and yaw motor torques results in a coupled 2
input - 2 output system. The experiment provides an economical
Hardware-in-the-Loop testbed to understand and develop control
laws for a vehicle that has dynamics representative of a tethered
rigid body helicopter, spacecraft or underwater vehicle.
2 DOF Helicopter
SPECIALTY CHALLENGE