- Lead Time:
- 6 to 9 months
- Mass:
- 1700 g
- Dimensions:
- 95.4 x 95.9 x 67.3 mm
- Operating Temperature:
- -45C to 85C
- Maximum Torque:
- 2 mN.m
- Magnetic Moment:
- 0.5 (X/Y), 0.4 (Z)
- Attitude Determination Accuracy:
- 30 arcseconds
- Pointing Accuracy:
- <0.1 deg
- Slew Rate:
- 1.5 deg/sec
- Radiation Tolerance:
- 45 krad
- Supply Voltage:
- 5 V (typ.)
- Maximum Power Consumption:
- 50 W
- Idle Power Consumption:
- 0.9 W
The iADCS400 matches the ST200 star tracker with Hyperion’s RW400-series of reaction wheels, as well as the MTQ400 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 5 standard CubeSat PCB’s, taking up 0.7U in terms of volume. With the help of the RW400-series of reaction wheels, it is capable of precisely pointing and slewing 6 to 12U 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.
Like all other integrated systems by Hyperion Technologies, the iADCS400 is stack-through, allowing users to place it anywhere in their satellite.
iADCS400
AAC HyperionThe iADCS400 matches the ST200 star tracker with Hyperion’s RW400-series of reaction wheels, as well as the MTQ400 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 5 standard CubeSat PCB’s, taking up 0.7U in terms of volume. With the help of the RW400-series of reaction wheels, it is capable of precisely pointing and slewing 6 to 12U 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.
Like all other integrated systems by Hyperion Technologies, the iADCS400 is stack-through, allowing users to place it anywhere in their satellite.
- Lead Time:
- 6 to 9 months
- Mass:
- 1700 g
- Dimensions:
- 95.4 x 95.9 x 67.3 mm
- Operating Temperature:
- -45C to 85C
- Maximum Torque:
- 2 mN.m
- Magnetic Moment:
- 0.5 (X/Y), 0.4 (Z)
- Attitude Determination Accuracy:
- 30 arcseconds
- Pointing Accuracy:
- <0.1 deg
- Slew Rate:
- 1.5 deg/sec
- Radiation Tolerance:
- 45 krad
- Supply Voltage:
- 5 V (typ.)
- Maximum Power Consumption:
- 50 W
- Idle Power Consumption:
- 0.9 W
The iADCS400 matches the ST200 star tracker with Hyperion’s RW400-series of reaction wheels, as well as the MTQ400 series of magnetorquers. Combined with Berlin Space Technologies’ flight-proven control algorithms, it offers an entirely autonomous attitude control system, in the space of 5 standard CubeSat PCB’s, taking up 0.7U in terms of volume. With the help of the RW400-series of reaction wheels, it is capable of precisely pointing and slewing 6 to 12U 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.
Like all other integrated systems by Hyperion Technologies, the iADCS400 is stack-through, allowing users to place it anywhere in their satellite.