The Cube Module Overview
Black, Green, BlueF4, PurpleF4 STM32F427; flash 2MB, RAM 256KB.
Yellow STM32F777; flash 2MB, Ram 512KB.
Orange, BlueH7, PurpleH7 STM32H753; flash 2MB, RAM 1MB.
On-board 16KB SPI FRAM
Black, Green, BlueF4, Purple MPU9250 16G integrated accelerometer / gyro.
Orange, BlueH7, ICM 20649 30G integrated accelerometer / gyro.
MS5611 Barometer
All sensors connected via SPI.
Micro SD interfaces via SDIO.
MPU9250, LSM303D, L3GD20 are all EOL, As such, all new designs should use the H7 based boards CubeBlueH7, CubeOrange, and CubePurpleH7 are 100% plug and play with all carrier boards that are compliant with our reference design dating back to 2014.
at the time of the latest edit here, cube PurpleF4 was still in stock, but when stocks run out, CubePurpleH7 will take its place.
LSM303D integrated accelerometer / magnetometer.
L3GD20 gyro.
MPU9250 Gyro / Accel
MS5611 Barometer
All sensors connected via SPI.
ICM20602
ICM 20948
MS5611 Barometer
All sensors connected via SPI.
14 PWM servo outputs (8 from IO, 6 from FMU).
R/C inputs for CPPM, Spektrum / DSM and S.Bus.
Analogue / PWM RSSI input.
S.Bus servo output.
5 general purpose serial ports, 2 with full flow control
Two I2C ports
One SPI port (un-buffered, for short cables only not recommended for use).
Two CAN Bus interface. (CAN FD for BlueH7 and Orange with CubePilot Logo)
3 Analogue inputs
High-powered piezo buzzer driver. (On expansion board)
High-power RGB LED. (I2C driver compatible Connected externally only)
Safety switch / LED.
The Cube continues with the FMU + IO architecture from the previous generation, incorporating the two functional blocks in a single physical module.
The Cube has eight PWM outputs that are connected to IO and can be controlled by IO directly via R/C input and on-board mixing even if FMU is not active (failsafe / manual mode). Multiple update rates can be supported on these outputs in three groups; one group of four and two groups of two. PWM signal rates up to 400Hz can be supported. These 8 PWM's are output ONLY and are capable of driving up to 50mA each, but only a total of 100mA for the 8.
Six PWM outputs are connected to FMU and feature reduced update latency. These outputs cannot be controlled by IO in failsafe conditions. Multiple update rates can be supported on these outputs in two groups; one group of four and one group of two.
PWM signal rates up to 400Hz can be supported.
All PWM outputs are EDS-protected, and they are designed to survive accidental mis-connection of servos without being damaged. The servo drivers are specified to drive a 50pF servo input load over 2m of 26AWG servo cable.
the I/O PWM outputs can also be configured as individual GPIOs. Note that these are not high-power outputs – the PWM drivers are designed for driving servos and similar logic inputs only, not relays or LEDs.
All peripherals are connected through a single 80 pin connector, and the peripherals are connected via a baseboard that can be customized for each application
The initial base board features separate connectors for each of the peripheral ports (with a few exceptions.
Five serial ports are provided. Serial 1 and 2 feature full flow control. Serial 3 is recommended as the GPS port and has the safety button and (possibly the safety led) as well as I2C for the compass and RGB LED. Serial 4 also has I2C, but on the second bus, thus allowing two compass modules to be connected at the same time. Serial 5 is available as a header underneath the board. Serial ports are 3.3V CMOS logic level, 5V tolerant, buffered and ESD-protected.
The SPI port is not buffered; it should only be used with short cable runs. Signals are 3.3V CMOS logic level, but 5V tolerant. SPI is only available to test points on the first base board, along with a CS and INT pin.
Analogue 1-3 are protected against inputs up to 12V, but scaled for 0-3.3V inputs. The RSSI input supports either PWM or analogue RSSI. This input shares a pin with S.Bus output - only one may be connected at a time.
CPPM, S.Bus and DSM/Spektrum input are unchanged from previous versions.
The CAN ports are standard CAN-Bus; termination for one end of the bus is fixed on- board. Drivers are on-board the FMU
The piezo port will drive most piezo elements in the 5 - 300nF range at up to 35V. it is intended to be extremely loud, with the achievable sound pressure level limited by the sensitivity of the piezo element being driven.
I2C is direct driven, un-buffered, and pulled up to *3.3v on-board* the FMU
Serial 5 is used for the on-board ADSB-IN receiver that is featured on newer carrier boards
All flight sensors in The Cube are connected via SPI.
CUBE TYPE | Life Cycle | IMU1 | IMU2 | IMU3 | Baro1 | Baro2 |
CubeBlack CubeBlueF4 CubeGreen | EOL | MPU9250 | LSM303D/L3GD20 | MPU9250 | MS5611 | MS6511 |
CubeBlack+ | EOL | MPU9250 | ICM20602 | ICM20948 | MS5611 | MS5611 |
CubePurpleF4 | EOL | MPU9250 | NA | NA | MS5611 | NA |
CubePurpleH7 | ACTIVE | ICM20649 | NA | NA | MS5611 | NA |
CubeOrange CubeYellow CubeBlueH7 | ACTIVE | ICM20649 | ICM20602 | ICM20948 | MS5611 | MS5611 |
IMU1, Non-Isolated IMU2 & 3, Isolated Data-ready signals from all sensors are NOT ROUTED on the Isolated IMU
The Cube removes the power management from the FMU, the Servo rail is no longer the primary source of backup power for the FMU, and it leaves it there for the IO last chance failsafe.
The supply of 3.3v
Split digital and analogue power domains for FMU and sensors.
Backup power for IO in the case of FMU power supply failure.
Key features of The Cube power architecture:
Single, independent 5V supply for the flight controller and peripherals.
Integration with *2 power bricks* or compatible alternative, including current and voltage sensing.
Low power consumption and heat dissipation.
Power distribution and monitoring for peripheral devices.
Protection against common wiring faults; under/over-voltage protection, overcurrent protection, thermal protection.
Brown-out resilience and detection.
Both FMU and IO operate at 3.3V, and each has its own private dual-channel regulator. As in The Cube (formerly known as Pixhawk), each regulator features a power-on reset output tied to the regulator’s internal power-up and drop-out sequencing.
Power may be supplied to The Cube via USB, via the power brick port, or the second brick port. Each power source is protected against reverse-polarity connections and back-powering from other sources.
The Cube F4 series FMU + IO power budget is 450mA, including all LEDs and the Piezo buzzer. Peripheral power is limited to 2.5A total. The Cube F7 and H7 series FMU + IO power budget is 550mA, including all LEDs and the Piezo buzzer. Peripheral power is limited to 2.5A total.
The increase in power budget is due to the improved heater on the cube orange
USB IS NOT RECOMMENDED IN FLIGHT ON Nuttx code
The brick port is the preferred power source for Cube, and brick power will always be selected if it is available.
The Cube supports both standard (5V) and high-voltage (up to 10V) servo power with some restrictions.
IO will accept power from the servo connector up to 10V. This allows IO to failover to servo power in all cases if the main power supply is lost or interrupted.
FMU and peripherals will NOT accept power from the servo connector.
The Cube introduces a backup power port; this is set up the same as the primary power input.
At input voltages over 5.7V power is locked out.
The Cube and peripherals combined may draw up to 2.75A total when operating on Aux power, provided that the Brick or other power source can supply the required current.
Power is never supplied by The Cube to servos.
The I/O chip takes power up to 10.5v from the servo rail; this is used to revert to manual mode in the unfortunate event that the other two main sources of power fail. This is only useful for plane, and only useful if the I/O chip has been mapped correctly.
Power from USB is supported for software update, testing and development purposes. USB power is supplied to the peripheral ports for testing purposes, however total current consumption must typically be limited to 500mA, including peripherals, to avoid overloading the host USB port.
When more than one power source is connected, power will be drawn from the highest-priority source with a valid input voltage.
In most cases, FMU should be powered via the power brick or a compatible off board regulator via the brick port or auxiliary power rail.
In desktop testing scenarios, taking power from USB avoids the need for a BEC or similar servo power source (though servos themselves will still need external power).
For each of the components listed, the input voltage ranges over which the device can be powered from each input is shown.
| Brick port | Aux port | USB port | Servo rail |
FMU | 4 - 5.7V | 4 - 5.7V | 4 - 5.7V | NIL |
IO | 4 - 5.7V | 4 - 5.7V | 4 - 5.7V | 4 - 10.5V |
Peripherals | 4 - 5.7 2.5A max | 4 - 5.7 2.5A max | 4 - 5.7 2.5A max | NIL |
The Cube provides power routing, over/under voltage detection and protection, filtering, switching, current-limiting and transient suppression for peripherals. Power outputs to peripherals feature ESD and EMI filtering, and the power supply protection scheme ensures that no more than 5.5V is presented to peripheral devices. Power is disconnected from the peripherals when the available supply voltage falls below 2.7V, or rises above approximately 5.7V.
Peripheral power is split into two groups:
Serial 1 (TELEM 1) has a private 1.5A current limit, intended for powering a low power. This output is separately EMI filtered and draws directly from the USB / Brick inputs. Peak power draw on this port should not exceed 1.5A, never power your telemetry from this port under any circumstance.
All other peripherals share a 1A current limit and a single power switch. Peak power draw on this port should not exceed 1.5A. Each group is individually switched under software control.
The Spektrum / DSM R/C interface draws power from its own regulator, rather than from either of the groups above. This port is switched under software control so that Spektrum / DSM binding can be implemented. Spektrum receivers generally draw ~25mA.
S.Bus and CPPM receivers are powered by a dedicated power supply. Please do not connect any servos to this power, only an RX by itself.
Both the FMU and IO microcontrollers feature Capacitor-backed real-time clocks and SRAM. The on-board backup Capacitor has capacity sufficient for the intended use of the clock and SRAM, which is to provide storage to permit orderly recovery from unintended power loss or other causes of in-air restarts. The capacitors are recharged from the FMU 3.3V rail. this will only function in the event of software existing to support this feature.
The battery voltage and current reported by both bricks can be measured by the FMU. In addition, the 5V unregulated supply rail can be measured (to detect brown- out conditions). IO can measure the servo power rail voltage.
Over-current conditions on the peripheral power ports can be detected by the FMU. Hardware lock-out prevents damage due to persistent short-circuits on these ports. The lock- out can be reset by FMU software. The under/over voltage supervisor for FMU provides an output that is used to hold FMU in reset during brown-out events.
EMI filtering is provided at key points in the system using high-insertion-loss pass- through filters. These filters are paired with TVS diodes at the peripheral connectors to suppress power transients.
Reverse polarity protection is provided at each of the power inputs. USB signals are filtered and terminated with a combined termination/TVS array.
Most digital peripheral signals (all PWM outputs, serial ports, I2C port) are driven using ESD-enhanced buffers and feature series blocking resistors to reduce the risk of damage due to transients or accidental misconnections.
Scope of this Document
This document covers the complete interface standard and core mechanical, electrical and external connection options of The Cube module series. Sections marked as LT (long term) are intended to be kept stable to isolate vehicle from autopilot revisions.
Interface Standard
Connector Series
Low density: 0.1” over mould Futaba keyed servo connectors (Mfg. to be identified)
Cabling: AWG24, ribbon or round, iconic colour scheme
Stack: Hirose DF17, 80pos , 4 mm stacking height, 0.5 mm pitch, drop-proof
High density: JST-GH 1.25 mm
Cabling: AWG28, ribbon, iconic colour scheme
Power Module: Molex Clik-Mate 2 mm for both main and backup power(on bottom of board?)
The Cube
Mechanical: 30x30 mm M3 mounting hole pattern, 35x35 mm footprint
80 position DF17 connector. Carries all autopilot interface connections.
Minimal (read: really minimal) electrical protection
No power management
3.8 to 5.7V operation (absolute maximum ratings)
4.0 to 5.5V operation (compliant rating)
The Cube IO
Total connectivity:
2x I2C
2x CAN: CAN1 and CAN2
4x UART: TELEM1, TELEM2, GPS (I2C 1 embedded), SERIAL4(I2C 2 embedded)
1x Console: CONSOLE (SERIAL5)
1x HMI: USB extender
Main Power - 6 pos (ClikMate 6 pos 2.0mm) | Connector：POWER1
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VDD_5V_BRICK | IN | 5 V | RED/GRAY | Supply To AP from Power Brick |
2 | VDD_5V_BRICK | IN | 5 V | RED/GRAY | Supply To AP from Power Brick |
3 | BATT_CURRENT_SENS_PROT | | 3.3 V | BLACK | Battery Current Connecter |
4 | BATT_CURRENT_VOLTAGE_PROT | IN | 3.3 V | BLACK | Battery Voltage Connecter |
5 | GND | - | GND | BLACK | GND connection |
6 | GND | - | GND | BLACK | GND connection |
Backup Power - 6 pos | Connector：POWER2
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VDD_5V_BRICK | IN | 5 V | RED/GRAY | Supply To AP from Power Brick |
2 | VDD_5V_BRICK | IN | 5 V | RED/GRAY | Supply To AP from Power Brick |
3 | AUX_BATT_CURRENT_SENS | - | 3.3 V | BLACK | Aux Battery Current Connecter |
4 | AUX_BATT_VOLTAGE_SENS | IN | 3.3 V | BLACK | Aux Battery Voltage Connecter |
5 | GND | - | GND | BLACK | GND connection |
6 | GND | - | GND | BLACK | GND connection |
I2C - 4 pos (1 fitted as a standalone, 1 old internal) | Connector：I2C2
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VCC_5V | OUT | 5 V | RED/GRAY | Supply to peripheral from AP |
2 | I2C_2_SCL | IN/OUT | 3.3 V (PULLUPS) | BLUE/BLACK | SCL, Pull-up on AP |
3 | I2C_2_SDA | IN/OUT | 3.3 V (PULLUPS) | GREEN/BLACK | SDA, Pull-up on AP |
4 | GND | | GND | BLACK | GND connection |
CAN (2 fitted) | Connector：CAN1, CAN2
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VCC_5V | OUT | 5 V | RED/GRAY | Supply to peripheral from AP |
2 | CAN_H | IN/OUT | 12 V | YELLOW/BLACK | CAN High |
3 | CAN_L | IN/OUT | 12 V | GREEN/BLACK | CAN Low |
4 | GND | - | GND | BLACK | GND connection |
UART GENERIC (autopilot side) | Connector : TELEM1, TELEM2
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VCC_5V | OUT | 5 V | RED/GRAY | Supply to peripheral from AP |
2 | MCU_TX | OUT | 3.3 V - 5.0 V TTL | YELLOW/BLACK | TX of AP |
3 | MCU_RX | IN | 3.3 V - 5.0 V TTL | GREEN/BLACK | RX of AP |
4 | MCU_CTS (TX) | OUT | 3.3 V - 5.0 V TTL | GRAY/BLACK | CTS (Clear To Send) |
5 | MCU_RTS (RX) | IN | 3.3 V - 5.0 V TTL | GRAY/BLACK | RTS (Request To Send) |
6 | GND | - | GND | BLACK | GND connection |
UART GPS (autopilot side, I2C is the original “External” bus), UART 3 | Connector：GPS1
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VCC_5V | IN | 5 V | RED | Supply to GPS from AP |
3 | GPS_RX | OUT | 3.3 V - 5.0 V TTL | BLACK | TX of AP |
2 | GPS_TX | IN | 3.3 V - 5.0 V TTL | BLACK | RX of AP |
4 | SCL | IN | 3.3 V | BLACK | I2C 1 SCL |
5 | SDA | IN/OUT | 3.3 V | BLACK | I2C 1 SDA |
6 | BUTTON | OUT | GND | BLACK | Signal shorted to GND on press |
7 | IO_LED_SAFET_PROT | OUT | GND | BLACK | LED Driver For Safety Button |
8 | GND | - | GND | BLACK | GND connection |
UART 4 (I2C2, the original “Internal” bus) | Port：GPS2
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | VCC_5V | OUT | 5 V | RED/GRAY | Supply to GPS from AP |
2 | MCU_TX | OUT | 3.3 V - 5.0 V TTL | YELLOW/BLACK | TX of AP |
3 | MCU_RX | IN | 3.3 V - 5.0 V TTL | GREEN/BLACK | RX of AP |
4 | SCL | OUT | 3.3 V - 5.0 V | GRAY/BLACK | I2C 2 SCL |
5 | SDA | IN | 3.3 V - 5.0 V | GRAY/BLACK | I2C 2 SDA |
6 | GND | - | GND | BLACK | GND connection |
UART 5 (Debug), S.Bus out - FR-SKY TELEM? or Debug | Port：CONS SBUSo
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | S.Bus_Out | OUT | | | S.Bus Signal Output, TX of AP |
2 | MCU_TX | OUT | 3.3 V - 5.0 V TTL | | TX of AP |
3 | VDD_SERVO | OUT | Servo Voltage | | Servo rail voltage |
4 | MCU_RX | IN | 3.3 V - 5.0 V TTL | | RX of AP |
5 | GND | - | GND | | GND connection |
6 | GND | - | GND | | GND connection |
Debug (New Standard Debug) (Digikey PN for housing SM06B-SURS-TF(LF)(SN)-ND)
IO DEBUG
Pin # | Name | I/O | Voltage | Wire Color | Description |
1 | VDD 5V PEIPH | OUT | 5 V | | 5V |
2 | IO_TX | OUT | 3.3 V - 5.0 V TTL | | TX of AP IO_uart1 TX |
3 | IO_RX | IN | 3.3V - 5.0 V TTL | | RX of AP IO_uart1 RX |
4 | IO-SWDIO | I/O | 3.3 V - 5.0 V TTL | | Serial wire debug I/O |
5 | IO-SWCLK | I/O | 3.3 V - 5.0 V TTL | | Serial wire Clock |
6 | GND | OUT | GND | | GND connection |
FMU DEBUG
Pin # | Name | I/O | Voltage | Wire Color | Description |
1 | VDD 5V PEIPH | OUT | 5 V | | 5V |
2 | FMU_TX (SERIAL 5) | OUT | 3.3 V - 5.0 V TTL | | TX of AP FMU_uart5 TX |
3 | FMU_RX (SERIAL 5) | IN | 3.3V - 5.0 V TTL | | RX of AP FMU_uart5 RX |
4 | FMU-SWDIO | I/O | 3.3 V - 5.0 V TTL | | Serial wire debug I/O |
5 | FMU-SWCLK | I/O | 3.3 V - 5.0 V TTL | | Serial wire Clock |
6 | GND | OUT | GND | | GND connection |
Analogue | Port：ADC
Pin # | Name | I/) | Voltage | Wire Color | Description |
1 | VDD_5V_Periph | OUT | | | |
2 | Pressure sense in | IN | | | |
3 | GND | - | | | GND connection |
IO USART 1 / DSM / Spektrum | Port：SPKT
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | IO_USART1_RX_SPECTRUM_DSM | IN | | | IO USART 1 RX, DSM INPUT |
2 | GND | - | GND | | GND |
3 | VDD_3V3_Spektrum | OUT | 3.3 V | | private Power Supply |
HMI (Buzzer, USB, LEDs) | Port：USB
Pin # | Name | I/O | Voltage | Wire Colour | Description |
1 | V BUS | OUT | 5 V | RED/GRAY | USB V BUS |
2 | OTG_DP1 | IN/OUT | 3.3 V | GREEN/BLACK | USB Data Positive (D+) |
3 | OTG_DM1 | IN/OUT | 3.3 V | RED/BLACK | USB Data Minus (D-) |
4 | GND | - | GND | BLACK | GND |
5 | BUZZER_OUT | OUT | Battery Voltage | GRAY/BLACK | VBAT (8.4 - 42 V) |
6 | FMU_LED_AMBER | OUT | | BLACK | Boot / Error LED (FW updates) |
Back Edge (may rearrange to suit PCB layout) | Port：RCIN MAIN OUT AUX OUT
SERVO HEADER (0.1”, 1/1/15 power layout)
Pin # | Name | I/O | Voltage | Wire Colour | Description |
S - 1 | FMU_CH1_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 2 | FMU_CH2_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 3 | FMU_CH3_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 4 | FMU_CH4_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 5 | FMU_CH5_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 6 | FMU_CH6_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 7 | IO_CH1_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 8 | IO_CH2_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 9 | IO_CH3_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 10 | IO_CH4_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 11 | IO_CH5_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 12 | IO_CH6_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 13 | IO_CH7_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 14 | IO_CH8_PROT | OUT | 3.3 V Servo Signal, Servo Rail Power | | PWM Signal |
S - 15 | PPM_SBUS_PROT | IN/OUT | 3.3 V / 4.5 V Powered | | PPM / S.Bus Signal |
The Cube 80-pin DF17 Connector (LONG TERM STANDARD!)
Pin # | Name | I/O | Description |
1 | FMU_SWDIO | I/O | FMU serial wire debug I/O |
2 | FMU_LED_AMBER | O | Boot error LED (drive only, controlled by FET) |
3 | FMU_SWCLK | O | FMU serial wire debug clock |
4 | I2C_2_SDA | I/O | I2C Serial Data Tx/Rx |
5 | EXTERN_CS | O | Chip select for external SPI (NC, just for debugging) |
6 | I2C_2_SCL | O | I2C Serial Clock Signal |
7 | FMU_!RESET | I | Reset pin for the FMU |
8 | PROT_SPARE_1 | | Spare |
9 | VDD_SERVO_IN | I | Power for last resort I/O failsafe |
10 | PROT_SPARE_2 | | Spare |
11 | EXTERN_DRDY | I | Interrupt pin for external SPI (NC, just for debugging) |
12 | SERIAL_5_RX | I | UART 5 RX (Receive Data) |
13 | GND | | System GND |
14 | SERIAL_5_TX | O | UART 5 TX (Transmit Data) |
15 | GND | | System GND |
16 | SERIAL_4_RX | I | UART 4 RX (Receive Data) |
17 | SAFETY | | Safety button input |
18 | SERIAL_4_TX | O | UART 4 TX (Transmit Data) |
19 | VDD_3V3_SPEKTRUM_EN | O | Enable for the Spektrum voltage regulator |
20 | SERIAL_3_RX | I | UART 3 RX (Receive Data) |
21 | PRESSURE_SENS_IN | AI | Analogue Signal port, for pressure sensor, Laser range finder, or Sonar |
22 | SERIAL_3_TX | O | UART 3 TX (Transmit Data) |
23 | AUX_BATT_VOLTAGE_SENS | AI | Voltage sense for Aux battery input |
24 | ALARM | O | Buzzer PWM Signal |
25 | AUX_BATT_CURRENT_SENS | AI | Current sense for Aux battery input |
26 | IO_VDD_3V3 | I | IO chip power, pinned through for debug |
27 | VDD_5V_PERIPH_EN | O | Enable voltage supply for Peripherals |
28 | IO_LED_SAFET_PROT | O | IO-LED_SAFETY (safety LED) pinned out for IRIS |
29 | VBUS | I | USB VBus (VDD) |
30 | SERIAL_2_RTS | | UART 2 RTS (Request To Send) |
31 | OTG_DP1 | I/O | USB Data+ (D) |
32 | SERIAL_2_CTS | | UART 2 CTS (Clear To Send) |
33 | OTG_DM1 | I/O | USB Data- (M) |
34 | SERIAL_2_RX | I | UART 2 RX (Receive Data) |
35 | I2C_1_SDA | I/O | I2C Serial Data Tx/Rx |
36 | SERIAL_2_TX | O | UART 2 TX (Transmit Data) |
37 | I2C_1_SCL | O | I2C Serial Clock Signal |
38 | SERIAL_1_RX | I | UART 1 RX (Receive Data) |
39 | CAN_L_2 | I/O | FMU CAN bus Low Signal Driver |
40 | SERIAL_1_TX | O | UART 1 TX (Transmit Data) |
41 | CAN_H_2 | I/O | FMU CAN bus High Signal Driver |
42 | SERIAL_1_RTS | | UART 1 RTS (Request To Send) |
43 | VDD_5V_PERIPH_OC | I | Error state message from Peripheral power supply |
44 | SERIAL_1_CTS | | UART 1 CTS (Clear To Send) |
45 | VDD_5V_HIPOWER_OC | I | Error state message from High power Peripheral power supply |
46 | IO_USART_1_TX | O | I/O USART 1 TX |
47 | BATT_VOLTAGE_SENS_PROT | AI | Voltage sense from main battery |
48 | IO_USART1_RX_SPECTRUM_DSM | O | Signal from Spectrum receiver |
49 | BATT_CURRENT_SENS_PROT | AI | Current sense from main battery |
50 | FMU_CH1_PROT | O | FMU PWM output channel 1 |
51 | SPI_EXT_MOSI | O | External SPI, for debug only |
52 | FMU_CH2_PROT | O | FMU PWM output channel 2 |
53 | VDD_SERVO | I | VDD_Servo, for monitoring servo bus |
54 | FMU_CH3_PROT | O | FMU PWM Output Channel 3 |
55 | VDD_BRICK_VALID | I | Main Power valid signal |
56 | FMU_CH4_PROT | O | FMU PWM Output Channel 4 |
57 | VDD_BACKUP_VALID | I | Backup Power valid Signal |
58 | FMU_CH5_PROT | O | FMU PWM Output Channel 5 |
59 | VBUS_VALID | I | USB bus valid signal |
60 | FMU_CH6_PROT | O | FMU PWM Output Channel 6 |
61 | VDD_5V_IN_PROT | I | Main power (5V) into FMU from power selection |
62 | PPM_SBUS_PROT | I | PPM / S.Bus Signal Input |
63 | VDD_5V_IN_PROT | I | Main power (5V) into FMU from power selection |
64 | S.BUS_OUT | O | S.Bus Signal Output |
65 | IO_VDD_5V5 | O | IO VDD 5.5 V |
66 | IO_CH8_PROT | O | I/O PWM Output Channel 8 |
67 | SPI_EXT_MISO | I | External SPI, for Debug only |
68 | IO_CH7_PROT | O | I/O PWM Channel 7 |
69 | IO_SWDIO | I/O | I/O serial wire debug |
70 | IO_CH6_PROT | O | I/O PWM Output Channel 6 |
71 | IO_SWCLK | O | I/O Serial Wire Debug Clock |
72 | IO_CH5_PROT | O | I/O PWM Output Channel 5 |
73 | SPI_EXT_SCK | O | External SPI, for Debug only |
74 | IO_CH4_PROT | O | I/O PWM Output Channel 4 |
75 | IO_!RESET | I | I/O Reset Pin |
76 | IO_CH3_PROT | O | I/O PWM Output Channel 3 |
77 | CAN_L_1 | I/O | FMU CAN bus Low Signal Driver |
78 | IO_CH2_PROT | O | I/O PWM Output Channel 2 |
79 | CAN_H_1 | I/O | FMU CAN bus High Signal Driver |
80 | IO_CH1_PROT | O | I/O PWM Output Channel 1 |
The Cube Series | Cube Orange | Cube Blue H7 | Cube Purple H7 | Cube Yellow | Cube Black+ | Cube Black | Cube Green | Cube Blue | Cube Purple F4 |
Processor | STM32H753 | STM32H753 | STM32H753 | STM32F777 | STM32F427 V3 | STM32F427 V3 | STM32F427 V3 | STM32F427 V3 | STM32F427 V3 |
Remote Signal | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM | PPM/SBUS/DSM |
I/O PWN Voltage | 3.3V/5V software selectable | 3.3V/5V software selectable | 3.3V/5V software selectable | 3.3V/5V software selectable | 3.3V | 3.3V | 5.4v | 3.3V | 3.3V |
Redundancy | Triple Redundancy | Triple Redundancy | N/A | Triple Redundancy | Triple Redundancy | Triple Redundancy | Triple Redundancy | Triple Redundancy | N/A |
Isolation system | Y | Y | N | Y | Y | Y | Y | Y | N |
Temp regulator | Y | Y | N | Y | Y | Y | Y | Y | N |
Number of Accelerometer | 3 | 3 | 1 | 3 | 3 | 3 | 3 | 3 | 1 |
Number of Gyroscope | 3 | 3 | 1 | 3 | 3 | 3 | 3 | 3 | 1 |
Number of Magnetometer | 1 | 1 | N/A | 1 | 2 | 3 | 3 | 3 | 1 |
Number of Barometer | 2 | 2 | 1 | 2 | 2 | 2 | 2 | 2 | 1 |
Original of Manufacturing | Taiwan | U.S.A | Taiwan | Taiwan | Taiwan | Taiwan | Taiwan | U.S.A | Taiwan |
Product lifecycle | Available | Available | Available | Available | EOL Please use Cube Orange | EOL Please use Cube Orange | EOL Please use Cube Orange | EOL Please use Cube Blue H7 | EOL Please use Cube Purple H7 |
Three IMU's
these consist of 2 on the IMU board
1 fixed to the FMU
Two onboard compasses Cube Black, Green, Blue
these consist of 1 on the IMU board
1 Fixed on the FMU
One onboard compass Cube Orange, Cube Yellow
Two Baros
1 on the IMU (this Baro will most likely be removed in favour of a dedicated external Barometer.
1 Fixed on the FMU
Dual Power input
This removes the option of redundancy from the Servo rail and replaces it with a dedicated second power plug
A dedicated power protection Zener diode and Fet have been added to protect from voltages over 5.6v being applied to Aux input 2
This is only on the "PRO" carrier board mini carrier board still draws the backup from the servo rail.
Dual external I2C
This allows for connection of items to either I2C port, potentially allowing two GPS / Mag units to be plugged in without the Mags conflicting.
Power monitoring pins are now routed to the I/O chip, these will allow for the logging of power events during an inflight reboot.
Brick OK, Backup OK, and FMU 3.3V are all connected to a digital pin on the I/O via a 220Ohm resister.
