ULYSSES In Space

 

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ULYSSES

Ulysses HISCALE Data Analysis Handbook

 

Chapter 4: Instrument Details

 

4.5 Data System

 

4.5.1 Requirements, Characteristics, and Features

 

The LAN data system is a microprocessor based data processor and command system for the low energy charged particle experiment. The data system performs several functions for the experiment. It controls the sampling intervals and modes of operation of the data collection devices. The varying spin rates and telemetry rates of the host spacecraft (S/C) are accounted for. It also performs arithmetic and compression routines to maximize the amounts of information available. To provide flexibility, it processes serial data commands received from the host S/C.

 

The structure of the data system is that of a small dedicated computer. It is shown in block diagram form in Figure 4.33. The data system is composed of three 6" x 6" integrated circuits which are all radiation hardened 4000 series and 1800 series CMOS devices, packaged as flat-packs.

 

Figure 4.33 Data system block diagram

 

Figure 4.33

 

The data system requires the following voltages and currents:

 

Voltage Pre Radiation
Current
Pre Rad
Power
Post Radiation
Power
Post-Rad Power
+10V±1/2 120mA 1.2W 150mA 1.5W
+10V±1/2 5mA 25mW 6mA 30mW
-6V±1/2 1mA 6mW 2mA 12mW
TOTAL   1.23W   1.54W

 

The clock frequency is 1.0 MHz. The data system is non-redundant, excepting the S/C interfaces. 

 

4.5.2 Data System Software

 

The main program is a polling loop which tests for occurrence of 9 flags, as shown in Figure 4.34. Preference is given to those functions which require the least timing delay. The initialization routine starts the data system in an operations state. An interrupt routine allows a new operating program to be loaded in the event of certain hardware failures.

 

The main routine calls subroutines to load commands, output data, and generate control signals. Three data processing routines are called to perform summation, compression, and sorting functions. The data format is fixed, regardless of the S/C telemetry rate.

 

Figure 4.34 Data system software block diagram. Click here for larger version (pdf file).

 

Figure 4.34

 

 

Next: Chapter 4.5.3: Format

 

Return to Chapter 4 Table of Contents

Return to Ulysses HISCALE Data Analysis Handbook Table of Contents


Updated 8/8/19, Cameron Crane

QUICK FACTS

Manufacturer: ESA provided the Ulysses spacecraft, NASA provided the power supply, and various others provided its instruments.

Mission End Date: June 30, 2009

Destination: The inner heliosphere of the sun away from the ecliptic plane

Orbit:  Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane