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Simplifying operations with an uplink/downlink integration toolkitThe Operations Engineering Lab (OEL) at JPL has developed a simple, generic toolkit to integrate the uplink/downlink processes, (often called closing the loop), in JPL's Multimission Ground Data System. This toolkit provides capabilities for integrating telemetry verification points with predicted spacecraft commands and ground events in the Mission Sequence Of Events (SOE) document. In the JPL ground data system, the uplink processing functions and the downlink processing functions are separate subsystems that are not well integrated because of the nature of planetary missions with large one-way light times for spacecraft-to-ground communication. Our new closed-loop monitoring tool allows an analyst or mission controller to view and save uplink commands and ground events with their corresponding downlinked telemetry values regardless of the delay in downlink telemetry and without requiring real-time intervention by the user. An SOE document is a time-ordered list of all the planned ground and spacecraft events, including all commands, sequence loads, ground events, significant mission activities, spacecraft status, and resource allocations. The SOE document is generated by expansion and integration of spacecraft sequence files, ground station allocations, navigation files, and other ground event files. This SOE generation process has been automated within the OEL and includes a graphical, object-oriented SOE editor and real-time viewing tool running under X/Motif. The SOE toolkit was used as the framework for the integrated implementation. The SOE is used by flight engineers to coordinate their operations tasks, serving as a predict data set in ground operations and mission control. The closed-loop SOE toolkit allows simple, automated integration of predicted uplink events with correlated telemetry points in a single SOE document for on-screen viewing and archiving. It automatically interfaces with existing real-time or non real-time sources of information, to display actual values from the telemetry data stream. This toolkit was designed to greatly simplify the user's ability to access and view telemetry data, and also provide a means to view this data in the context of the commands and ground events that are used to interpret it. A closed-loop system can prove especially useful in small missions with limited resources requiring automated monitoring tools. This paper will discuss the toolkit implementation, including design trade-offs and future plans for enhancing the automated capabilities.
Document ID
19950011147
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murphy, Susan C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Miller, Kevin J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Guerrero, Ana Maria
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Joe, Chester
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Louie, John J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Aguilera, Christine
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Publication Information
Publication: NASA. Goddard Space Flight Center, Third International Symposium on Space Mission Operations and Ground Data Systems, Part 2
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
95N17562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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