Attitude and heading reference system (AHRS) is a device that utilizes MEMS inertial sensors (accelerometers, gyroscopes) and magnetometers, combined with advanced sensor fusion algorithms (most commonly Kalman filtering and its variants), to calculate real-time attitude information (pitch angle, roll angle, yaw/heading angle) of a carrier (aircraft, vehicle, ship, robot, etc.) relative to the local horizontal plane and in the north direction.
In the attitude stabilization and control system of unmanned aerial vehicles, the flight control system relies on real-time, high-frequency attitude data provided by AHRS to stabilize the aircraft, perform maneuvers (such as turning, climbing, descending), and maintain hovering. This is the most core application of AHRS in unmanned aerial vehicles. Meanwhile, the heading angle provided by AHRS is a key input for unmanned aerial vehicle integrated navigation systems (usually integrated with GPS, barometers, etc.), used for waypoint tracking and autonomous navigation.
In the control applications of general aviation aircraft (small aircraft, helicopters), AHRS provides attitude indication and magnetic heading information on the primary flight display (PFD) for pilots. The integration of AHRS with GPS and other systems can provide more reliable and robust navigation solutions for general aviation aircraft.
In the stability control of ground vehicles, AHRS is used to detect the roll angle and yaw rate of the vehicle, prevent sideslip and rollover, and provide the auto drive system with vehicle attitude information relative to the road surface for path planning, control decision-making and sensor fusion (such as fusion with camera and radar data).
AHRS monitors the roll and pitch angles of ships for navigation safety, cargo management, or scientific research purposes. In the stability control system of a ship, attitude feedback is provided for stabilizing devices such as anti roll fins and gyro anti roll devices. In ship autopilot/trajectory control, providing heading information is the foundation of ship autopilot.
AHRS provides attitude and heading information for ground, aerial, or underwater robots during mobile robot navigation, which is crucial for autonomous movement and positioning. In a robotic arm control system, sensing the posture of the end effector or joint of the robotic arm.
In AR/VR systems, the VR headset is equipped with AHRS to track changes in the user's head posture and update the virtual scene perspective. Simultaneously used to capture posture movements of body parts or props (usually requiring higher accuracy and using more professional IMUs).
AHRS has the following irreplaceable advantages:
→ Low cost: The large-scale production of MEMS technology makes AHRS much cheaper than high-precision fiber optic or laser gyro inertial navigation systems (INS), making it widely applicable in consumer and commercial markets such as drones and automotive electronics.
→ Small size, light weight, low power consumption: MEMS sensors are very compact, and the entire AHRS module can be made very compact and lightweight, with relatively low power consumption, making it very suitable for platforms with limited space, weight, and power consumption (such as small drones and wearable devices).
→ Quick start and high dynamic response: After starting, it can quickly provide accurate attitude information within seconds to tens of seconds (depending on the convergence speed of the algorithm), without the need for long warm-up periods like mechanical gyroscopes. Capable of quickly responding to the intense maneuvering of the carrier, outputting high-frequency attitude data (usually up to 100Hz or higher), meeting the requirements of real-time control.
→ Easy to integrate: Typically provides standardized digital interfaces (such as UART, SPI, I2C, CAN, RS232, RS422) for easy integration with other systems (such as flight control computers, navigation computers, displays).
The following are the performance indicators of the AHRS series products.
Main Parameter |
A500 |
A5500 |
Unit |
|
Attitude angles
|
Heading angle |
0.2 |
0.1 |
° RMS |
Pitch/Roll angle |
0.2 |
0.1 |
° RMS |
|
Attitude ranges |
Roll |
±180 |
±180 |
° RMS |
Pitch |
±90 |
±90 |
° RMS |
|
Gyroscope |
||||
Measurement range |
±100 |
±2000 |
°/s |
|
Angle random walk |
0.09 |
0.6 |
°/√h |
|
Zero bias stability (In-Run) |
3 |
5.1 |
°/h (Allan) |
|
Accelerometer |
||||
Measurement range |
±10/±20/±40 |
±12 |
g |
|
Angle random walk |
0.03 |
0.08 |
(m/s)/√h |
|
Zero bias stability (In-Run) |
0.03 |
0.06 |
mg |
|
Magnetometer |
||||
Measurement range |
±8 |
±8 |
Gauss |
AHRS, with its core characteristics of solid-state, low cost, small size, low power consumption, and fast start-up, has become a core attitude sensing device in many fields such as modern drone flight control, small aircraft avionics upgrades, vehicle stability control, ship attitude monitoring and navigation, robot navigation, and VR/AR. Although its absolute accuracy is usually lower than high-end INS systems, its excellent cost-effectiveness and environmental adaptability make it the most widely used attitude reference solution.
Xml política de Privacidade blog Mapa do site
Direitos autorais
@ Micro-Magic Inc. Todos os direitos reservados.
SUPORTADO POR REDE