Design of a standard test and simulation assembly for a modular attitude and orbit control system (MACS): part I: phase 1 study report

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Abstract

A standard test and simulation assembly (TSA) for a modular attitude and orbit control system (MACS) is defined. Its functional requirements, detailed specification and design are presented. The assembly consists of a commercial available minicomputer and a specificly designed front-end which interfaces with the AOCS via an OBDH-, MACS- and IEEE- test bus. The standard ETOL software is to be used after some modifications.

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NLR_TR_83148_L_PART_I.pdf
(pdf | 55.2 Mb)

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