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Telemetry Ranging - Concept Paper SummaryBackground - Previous CCSDS meetings: Spring 2015: Telemetry ranging technique was described; Fall 2015: A comparison to GMSK (Gaussian Minimum Shift Keying) plus PN (Pseudo-random Noise) ranging was made. -How telemetry ranging works: The spacecraft tracks the phase of the uplink PN ranging signal; Receive-time of downlink telemetry frame provides timing information; No downlink ranging signal is used. - This presentation: Summarizes the telemetry ranging concept paper. - Purpose: The purpose of the concept paper is to propose that the RFM (Radio Frequency Multiplier) Working Group consider telemetry ranging for inclusion as a recommended method for two-way ranging in the 401.0-B Blue Book.
Document ID
20190028556
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Hamkins, Jon
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2019
Publication Date
April 6, 2016
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
JPL-CL-16-1281
Report Number: JPL-CL-16-1281
Meeting Information
Meeting: Spring 2016 CCSDS (Consultative Committee for Space Data Systems) Spring Technical Meetings
Location: Cleveland, OH
Country: United States
Start Date: April 4, 2016
End Date: April 8, 2016
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Other

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