Summary

The NanoAvionics Payload Controller 1.5 is a subsystem designed to interface between the payloads and NanoAvionics CubeSat bus. The controller provides a number of different interfaces for payload connection and can buffer data from payloads. It also controls the S-Band transmitter or transceiver to transmit the buffered data to ground Station.

Key features

  • Cortex™ M7 core
  • microSD NAND Memory support
  • Three On-Board PWM Controlled H-Bridges
  • PWM Outputs
  • FreeRTOS
  • In-Orbit firmware update
  • Firmware Power-on-check and Restore
  • RFS – Redundant Record-based File System
  • A number of Payload dedicated interfaces:
    • 100BASE-TX Ethernet port
    • CAN Interface
    • 2 x RS422 (on request interchangeable with 2 x RS485)
    • 3 x buffered SPI
    • 2 x USART/UART
    • 2 x I2C
  • CSP Support
  • Self-Diagnostics
  • Dynamic CPU Frequency Control
  • User-friendly Console

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Last updated: 2022-06-06

Payload Controller 1.5

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Specs

mass
65 g (typical)
length
95.50 ± 0.10
width
89.00 ± 0.10
height
12.21 mm
processor type
ARM® Cortex-M7 32 bit
processor clock
200 MHz typ. (configurable up to 400 MHz)
RAM
1 MB
4 MB SRAM (FMC-connected)
FRAM
512 kB (FMC-connected)
2x 512 kB (SPI) for frequently changing data storage
flash memory
2 MB (internal)
data storage
256 MB external NOR-FLASH (2×2 die, 64 MB each, QSPI)
up to 2x 32 GB microSD
data interface
CAN
2x RS422 (on request interchangeable with 2x RS485)
3x buffered SPI
2x buffered USART/UART
2x I2C
100BASE-TX Ethernet Port
operating temperature
-40 to 85 C
storage temperature
-40 to 85 C
radiation tolerance
20 krad
shock1
80 G
vibration2
14 Grms

1. 2 ms half-sine pulse, according to NASA GEVS 7000 standard

2. according to NASA GEVS 7000 standard)

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