CubeSats utilize standardized communication protocols for telemetry and control
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Peer-reviewed literature and reference encyclopedias confirm that CubeSat missions utilize established standardized communication protocols, such as UART, European Space Agency standards, and the CubeSat Space Protocol, for telemetry and command control.
The traditional CubeSats development model is a one-off build designed to accomplish a specific mission using proprietary hardware and software. The specific mission requirements and associated development costs result in a lack of reproducibility for CubeSats. The Naval Academy Standard Bus (NASB) advances the concept of CubeSat modularity with a design that physically separates a fully-functional standalone 1U bus from an independently-developed 1U or 2U customer payload module with a 10-pin wiring harness serving as the sole electrical interface between bus and payload modules. Residing within the standard bus module the main onboard computer (OBC) handles uplink and downlink communications and connects the NASB to the payload module through two interface boards: the Bus Board and the Payload Interface Board (PIB). Ground commands received by the NASB pass through the Bus Board to the PIB in the payload module, through which they are communicated to the payload via universal asynchronous receiver/transmitter (UART) protocol. Messages and stored data generated by the payloads are stored on a secure digital card within the PIB, to be passed on to NASB and downlinked to the ground station. This modular design allows for independent development of payloads, shortening CubeSat development timeline by eliminating the need for bus development in parallel with payload development.
Alenia Space España S.A. using ESA protocols such as ECSS-E-70-41A for ground communication, control and telemetry. The satellite was launched on 21 November
OPTOS was a Spanish nanosatellite designed and developed by INTA with support from the European Cooperation for Space Standardization (ECSS) as a low-cost technology demonstrator. It was launched in 2013 and had a service life of three years.
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A graphical user interface is proposed to facilitate telemetry collection and configuration set-up for CubeSat Space Protocol-compatible nanosatellites during their testing and assembly stage. The graphical user interface connects to the various subsystems of the nanosatellite through a module that functions as a gateway. The graphical user interface is written in Python and Qt. Python is an interpreted high-level language compatible with Linux systems, and Qt is a multi-platform graphical user interface development framework. Through the graphical user interface, telemetry from the various satellite modules can be collected.
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