Introduction
ER-AMM-2 is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of ER-AMM-2 attitude measurement module. With the built-in accelerometer sensor and gyroscope, ER-AMM-2 can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity.
ER-AMM-2 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication. Default baud rate 921600 (customized). With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer's original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.
A simple operation is required to connect our products to your system and obtain data without the 15-pin plug provided by our company.
Features
Attitude measurement type module
MEMS gyros and MEMS accelerometer
Low-cost and high reliability
Low power consumption
OEM modular design, several shapes optional
Application
Robotic control & orientation in autonomous machines, unmanned vehicles
Azimuth, attitude, position measuring and keeping in GNSS-assisted INS
Pitch, roll measuring in AHRS for UAV
Motion survey and keeping in MRU
Stabilizing & pointing in satellite antenna
Specifications
| Parameters | ER-AMM-201 | ER-AMM-202 | Unit |
| Gyro | |||
| Input Range | 400 | 400 | dps |
| Scale factor | 16000 | 20000 | LSB/°/s |
| Scale factor non-linearity | <50 | 200 | ppm |
| Scale factor temp drift (1σ) | 300 | 500 | ppm |
| Scale factor repeatability (1σ) | <300 | <10 | ppm |
| Bias temp drift (1б) | 50 | 50 | dph |
| Bias temp drift (1б) (After temp compensation) | <10 | 20 | dph |
| Bias stability (1б 10s) | <3 | 5 | dph |
| Bias stability (1б 1s) | <9 | 15 | dph |
| Bias Repeatability | <3 | 5 | dph |
| Accelerometer |
| Range | 30 | g |
| Bias Stability (10s 1σ) | <50 | ug |
| Bias Repeatability | 100 | ug |
| Bias Temp Coefficient | <20 | ug/℃ |
| Bias Temp Hysteresis | <1.5 | mg |
| Scale Factor Non-linearity | <500 | ppm |
| Scale Factor Repeatability | <30 | ppm |
| Scale Factor Temp Coefficient | 10 | ppm/℃ |
| Class II Non-linearity Coefficient | <100 | ug/g² |
| Scale Factor | 250000 | Lsb/g |
| Environment and power | ||
| Operate temperature | -40~+80 | ℃ |
| Storage temperature | -55~+105 | ℃ |
| Power supply | 6~12V | V |
| Power (power supply 6V) | 2 | W |
| Communication interface | RS-422 | |
| Physical characteristics | ||
| Size | A :70*65*45mm
B: 38.6 x 44.8 x 25.5mm
C:47×44×14mm:
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| Weight | A : ≤220g(withshell)
≤100g(without shell and baseboard) B: ≤70g C:≤40g |
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Application Techniques
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