Work

Verification of a CubeSat via hardware-in-the-loop simulation

Year: 2014

Type: article

Abstract: This paper describes the hardware-in-the-loop (HIL) simulation methodology used for the verification of functional requirements of e-st @r-I CubeSat. The satellite's behavior is investigated via HIL simulation, and the results obtained are consistent with the expected values in any operative conditions. It is proven that HIL simulation is a valuable means for supporting the verification process of small satellites and may help reduce the time and cost of the development phase and increase mission reliability.

Source: IEEE Transactions on Aerospace and Electronic Systems

DOI: 10.1109/taes.2014.130370

Authors: Sabrina Corpino, Fabrizio Stesina

Institution: Politecnico di Torino

Language: English

Topic: Spacecraft Design and Technology

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

Funder: Politecnico di Torino

OpenAlex ID: W2086270936