JPL Technical Report Server

Communicating by doppler : detecting spacecraft dynamics during critical maneuvers

Show simple item record

dc.contributor.author Asmar, Sami W.
dc.date.accessioned 2012-12-13T16:15:56Z
dc.date.available 2012-12-13T16:15:56Z
dc.date.issued 2012-06-12
dc.identifier.citation SpaceOps Conference, Stockholm, Sweden, June 11-15, 2012. en_US
dc.identifier.clearanceno 12-2315
dc.identifier.uri http://hdl.handle.net/2014/42522
dc.description.abstract Communicating information from spacecraft in deep space utilizes sophisticated techniques of modulations onto a microwave signal carrier. Under most conditions, there is a high success rate of sending commands to the spacecraft and receiving science data acquired by on-board instruments along with health and status information. There are conditions, however, where the signal dynamics are too high and/or the received signal-to-noise ratio is below the receiver threshold. Under these conditions, often by design and sometimes as a result of planned or unplanned critical maneuvers, events (e.g., orbit insertion or descent and landing), safe mode, etc., it becomes highly critical but exceedingly challenging to receive information about the health and dynamical behavior of the spacecraft. The Deep Space Network, being a world-class instrument for Radio Science research, developed openloop receivers, called the Radio Science Receiver, designed to capture the raw incoming electromagnetic signals and associated noise for Radio Science experiments; post data capture digital signal processing extracts the signal carrier for scientific analysis. This receiver provides a high level of configuration flexibility and can be optimized for the various types of experiments. In addition to its scientific utility, it proved to be useful, and in some cases critical, for the support of missions during specific scenarios were the link budget is below the threshold of the tracking receiver to maintain lock or the frequency dynamics are faster than the limits of the tracking receiver. In these cases, the signal carrier is often detected only in the open-loop receiver to provide information on the specific behavior of the spacecraft from the carrier dynamics. This paper describes the utility of the system to support mission-critical events for the three cases of Cassini’s Saturn orbit insertion, Huygens Titan landing, and Mars rovers landing. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012. en_US
dc.subject radio science en_US
dc.subject Radio Science Receiver (RSR) en_US
dc.subject mission-critical events en_US
dc.title Communicating by doppler : detecting spacecraft dynamics during critical maneuvers en_US
dc.type Preprint en_US
dc.subject.NASATaxonomy Space Communications, Spacecraft Communications, Command and Tracking en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account