- Lead Time:
- 6 to 9 months
- Mass:
- 470 g
- Dimensions:
- 95 x 90 x 32 mm
- Operating Temperature:
- -45C to 85C
- Attitude Determination Accuracy:
- 30 arcseconds (3σ)
- Nominal Torque:
- > 0.087 mN.m
- Nominal Magnetic Moment:
- 0.2 (X, Y), 0.1 (Z)
- Pointing Accuracy:
- < 1 deg
- Slew Rate:
- > 1.5 deg/sec
- Radiation Tolerance:
- > 45 krad
- Maximum Power Consumption:
- 4500 mW
- Idle Power Consumption:
- 1150 mW
- Supply Voltage:
- 5 V (typ.)
The iADCS200 matches the ST200 star tracker with RW210 series of reaction wheels, as well as the MTQ200 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 2 standard CubeSat PCB’s. With the help of the RW210 series of reaction wheels, it is capable of precisely pointing and slewing 1 to 4U CubeSats or platforms with similar moments of inertia.
It features a host of operating modes, chief among which is the target tracking mode, which allows users to enter latitude and longitude of a point on Earth, after which the system will orient a pre-defined instrument-side towards that target, following it until it has passed the local horizon.
The iADCS200 is also stack-through, allowing users to place it anywhere in their satellite.
iADCS200
AAC HyperionThe iADCS200 matches the ST200 star tracker with RW210 series of reaction wheels, as well as the MTQ200 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 2 standard CubeSat PCB’s. With the help of the RW210 series of reaction wheels, it is capable of precisely pointing and slewing 1 to 4U CubeSats or platforms with similar moments of inertia.
It features a host of operating modes, chief among which is the target tracking mode, which allows users to enter latitude and longitude of a point on Earth, after which the system will orient a pre-defined instrument-side towards that target, following it until it has passed the local horizon.
The iADCS200 is also stack-through, allowing users to place it anywhere in their satellite.
- Lead Time:
- 6 to 9 months
- Mass:
- 470 g
- Dimensions:
- 95 x 90 x 32 mm
- Operating Temperature:
- -45C to 85C
- Attitude Determination Accuracy:
- 30 arcseconds (3σ)
- Nominal Torque:
- > 0.087 mN.m
- Nominal Magnetic Moment:
- 0.2 (X, Y), 0.1 (Z)
- Pointing Accuracy:
- < 1 deg
- Slew Rate:
- > 1.5 deg/sec
- Radiation Tolerance:
- > 45 krad
- Maximum Power Consumption:
- 4500 mW
- Idle Power Consumption:
- 1150 mW
- Supply Voltage:
- 5 V (typ.)
The iADCS200 matches the ST200 star tracker with RW210 series of reaction wheels, as well as the MTQ200 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 2 standard CubeSat PCB’s. With the help of the RW210 series of reaction wheels, it is capable of precisely pointing and slewing 1 to 4U CubeSats or platforms with similar moments of inertia.
It features a host of operating modes, chief among which is the target tracking mode, which allows users to enter latitude and longitude of a point on Earth, after which the system will orient a pre-defined instrument-side towards that target, following it until it has passed the local horizon.
The iADCS200 is also stack-through, allowing users to place it anywhere in their satellite.