Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor
Microwave tracking, usually performed by on ground processing of the signals coming from a spacecraft, represents a crucial aspect in every deep-space mission. Various noise sources, including receiver noise, affect these signals, limiting the accuracy of the radiometric measurements obtained from t...
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doaj-9210120decfd41b7afacc6f49d5f215e2020-11-24T21:35:13ZengMDPI AGApplied Sciences2076-34172019-07-01914290910.3390/app9142909app9142909Hardware Prototyping and Validation of a W-ΔDOR Digital Signal ProcessorGian Carlo Cardarilli0Luca Di Nunzio1Rocco Fazzolari2Daniele Giardino3Marco Matta4Marco Re5Luciano Iess6Fabio Cialfi7Giorgio De Angelis8Dario Gelfusa9Ascanio Patrizio Pulcinelli10Lorenzo Simone11Department of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Electronic Engineering, University of Rome Tor Vergata, 00133 Roma, ItalyDepartment of Mechanical and Aerospace Engineering, University of Rome La Sapienza, 00184 Roma, ItalyThales Alenia Space Italia, Via Saccomuro, 24, 00131 Roma RM, ItalyThales Alenia Space Italia, Via Saccomuro, 24, 00131 Roma RM, ItalyThales Alenia Space Italia, Via Saccomuro, 24, 00131 Roma RM, ItalyThales Alenia Space Italia, Via Saccomuro, 24, 00131 Roma RM, ItalyThales Alenia Space Italia, Via Saccomuro, 24, 00131 Roma RM, ItalyMicrowave tracking, usually performed by on ground processing of the signals coming from a spacecraft, represents a crucial aspect in every deep-space mission. Various noise sources, including receiver noise, affect these signals, limiting the accuracy of the radiometric measurements obtained from the radio link. There are several methods used for spacecraft tracking, including the Delta-Differential One-Way Ranging (<inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR) technique. In the past years, European Space Agency (ESA) missions relied on a narrowband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR system for navigation in the cruise phase. To limit the adverse effect of nonlinearities in the receiving chain, an innovative wideband approach to <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR measurements has recently been proposed. This work presents the hardware implementation of a new version of the ESA X/Ka Deep Space Transponder based on the new tracking technique named Wideband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR (W-<inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR). The architecture of the new transponder guarantees backward compatibility with narrowband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR.https://www.mdpi.com/2076-3417/9/14/2909ΔDORW-ΔDORspacecraft tracking |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Gian Carlo Cardarilli Luca Di Nunzio Rocco Fazzolari Daniele Giardino Marco Matta Marco Re Luciano Iess Fabio Cialfi Giorgio De Angelis Dario Gelfusa Ascanio Patrizio Pulcinelli Lorenzo Simone |
spellingShingle |
Gian Carlo Cardarilli Luca Di Nunzio Rocco Fazzolari Daniele Giardino Marco Matta Marco Re Luciano Iess Fabio Cialfi Giorgio De Angelis Dario Gelfusa Ascanio Patrizio Pulcinelli Lorenzo Simone Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor Applied Sciences ΔDOR W-ΔDOR spacecraft tracking |
author_facet |
Gian Carlo Cardarilli Luca Di Nunzio Rocco Fazzolari Daniele Giardino Marco Matta Marco Re Luciano Iess Fabio Cialfi Giorgio De Angelis Dario Gelfusa Ascanio Patrizio Pulcinelli Lorenzo Simone |
author_sort |
Gian Carlo Cardarilli |
title |
Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor |
title_short |
Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor |
title_full |
Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor |
title_fullStr |
Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor |
title_full_unstemmed |
Hardware Prototyping and Validation of a W-ΔDOR Digital Signal Processor |
title_sort |
hardware prototyping and validation of a w-δdor digital signal processor |
publisher |
MDPI AG |
series |
Applied Sciences |
issn |
2076-3417 |
publishDate |
2019-07-01 |
description |
Microwave tracking, usually performed by on ground processing of the signals coming from a spacecraft, represents a crucial aspect in every deep-space mission. Various noise sources, including receiver noise, affect these signals, limiting the accuracy of the radiometric measurements obtained from the radio link. There are several methods used for spacecraft tracking, including the Delta-Differential One-Way Ranging (<inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR) technique. In the past years, European Space Agency (ESA) missions relied on a narrowband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR system for navigation in the cruise phase. To limit the adverse effect of nonlinearities in the receiving chain, an innovative wideband approach to <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR measurements has recently been proposed. This work presents the hardware implementation of a new version of the ESA X/Ka Deep Space Transponder based on the new tracking technique named Wideband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR (W-<inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR). The architecture of the new transponder guarantees backward compatibility with narrowband <inline-formula> <math display="inline"> <semantics> <mo>Δ</mo> </semantics> </math> </inline-formula>DOR. |
topic |
ΔDOR W-ΔDOR spacecraft tracking |
url |
https://www.mdpi.com/2076-3417/9/14/2909 |
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