Level-0 telemetry collection for spacecraft command and data handling subsystems

Author

Epperly, Michael E. ; Walls, Buddy J.

Author_Institution

Southwest Res. Inst., San Antonio, TX, USA

Volume

5

fYear

2001

fDate

2001

Firstpage

2191

Abstract

This paper presents the continuing development of flexible Level-0 command and telemetry collection hardware. Results of the requirements analysis, systems design and hardware fabrication and test are presented in detail. The objective of this research program was to provide a module that could handle a variety of interfaces accessible from either a spacecraft´s main computer or an on-board microcontroller. The module must serve as a level-0 “safe” mode processor and be able to execute commands received from the ground. The system designed as a result of this IR&D will be used in those applications where a critical need exists for a level-0 “safe” mode processor. The design may also be used to speed up system throughput by way of parallel processing with the main computer

Keywords

aerospace computing; aerospace control; command and control systems; data handling; microcontrollers; parallel processing; radiation hardening (electronics); space telemetry; space vehicle electronics; system buses; systems analysis; SEU; VME bus; flexible collection hardware; flexible interface capability; hardware fabrication; hardware test; level-0 telemetry collection; on-board microcontroller; parallel processing; requirements analysis; safe mode processor; spacecraft command and data handling subsystem; spacecraft control; systems design; Application software; Computer interfaces; Fabrication; Hardware; Microcontrollers; Process design; Space vehicles; System analysis and design; System testing; Telemetry;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace Conference, 2001, IEEE Proceedings.

Conference_Location

Big Sky, MT

Print_ISBN

0-7803-6599-2

Type

conf

DOI

10.1109/AERO.2001.931176

Filename

931176