Design of Constellations for Earth Observation with Intersatellite Links (original) (raw)

Optical intersatellite links for navigation constellations

International Conference on Space Optics — ICSO 2018

Satellite constellations are used for navigation purposes since long. Connecting the satellites in a constellation by intersatellite links (ISLs) offers a full range of new possibilities. Ranging and time synchronization information can be exchanged between the satellites to improve the in orbit SC positioning knowledge. Besides ranging and time synchronization, ISLs can be used for service channel purposes or to distribute SW updates for the spacecrafts in a short period of time. ISLs improve the navigation constellations autonomy properties being less vulnerable to ground station unavailabilities. For ISLs, radio frequency (RF) and optical technologies have been investigated. Due to the shorter wavelength, a better ranging resolution can be achieved with optical than with RF ISL solutions. Optical ISLs (OISLs) offer a very attractive solution for intersatellite links in terms of size, weight and power while providing multi gigabit per second data rate capabilities. In addition, optical communication links offer high operational security and immunity to interference sources while benefitting from a non-regulated optical frequency spectrum. For those reasons, optical intersatellite links for navigation constellations have been investigated in several studies supported by DLR and ESA. TESAT with partners have investigated the benefit of OISLs for navigation systems and on the Galileo OISL Terminal design. In this paper, the results of these studies will be presented. Various OISL connection schemes in a navigation constellation are compared. The key design parameters of a Laser Communication Terminal for navigation systems will be given. Furthermore, the results of a lab demonstration showing the parallel distribution of ranging and communication data will be summarized. The focus of the investigation is on the Galileo navigation constellation.

The european satellite navigation system Galileo

Wuhan University Journal of Natural Sciences, 2003

This paper starts with a brief discussion of the Galileo project status and with a description of the present Galileo architecture (space segment, ground segment, user segment). It focuses on explaining special features compared to the American GPS system. The presentation of the user segment comprises a discussion of the actual Galileo signal structure. The Galileo carder frequency, modulation scheme and data rate of all 10 navigation signals are described as well as parameters of the search and rescue service. The navigation signals are used to realize three types of open services, the safety of life service, two types of commercial services and the public regulated service. The signal performance in terms of the pseudorange code error due to thermal noise and multipath is discussed as well as interference to and from other radionavigation services broadcasting in the F_,5 and E6 frequency band. The interoperability and compatibility of Galileo and GPS is realized by a properly chosen signal structures in E5a/L5 and E2-L1-E1 and compatible geodetic and time reference frames. Some new results on reciprocal GPS/Galileo signal degradation due to signal overlay are presented as well as basic requirements on the Galileo code sequences.

Overview of Galileo System

Signals and Communication Technology, 2014

This chapter provides an introduction to the Galileo program and architecture. It starts by presenting the program context, rationale and history, including the early definition phases and test beds and the GIOVE experimental satellites. It then presents an overview of the Galileo services. Later, an architectural overview is provided, including the Galileo segments: the Space Segment, the Ground Mission Segment, and the Ground Control Segment. The chapter also provides a description of Galileo's contribution to the Search And Rescue services through COSPAS/SARSAT, and finalizes with an overview of the user segment and highlighting interoperability and compatibility issues with other GNSS.

The Galileo Project and Scientific Applications

A short overview of the European Satellite navigation programme Galileo and its current state of development is provided, followed by a brief description of scientific applications of navigation signals in general and the expectations for Galileo in particular.

GALILEO system overview

Acta Astronautica, 2004

This paper presents a brief description of the GALILEO services and summarizes the main performance parameters. The current status of the system architecture deÿnition is presented in a concise overall view on the various elements of the system and their functions with a main focus on the GALILEO ground segment.

Galileo in Maritime Applications

2005

The past decade has seen the continued growth of GPS and its many different applications. The European Union and the European Space Agency has announced the development of the European Global Navigation Satellite System – Galileo. Clearly acceptance of additional satellite systems into markets that successfully use GPS will require identification of those key areas where Galileo is capable of providing added-value, either standalone or more likely as a component of an overall integrated suite of navigation systems. These key areas are often termed the key differentiators for Galileo. This paper introduces three projects; GALEWAT, MARGAL and GEM. The GALEWAT project is fully funded by the European Space Agency (ESA), while MARGAL is 50% co-funded and GEM fully funded by the European Union (EU) through the Sixth Framework Research and Development Programme which is being administered on behalf of the EU by the Galileo Joint Undertaking (GJU). The overall aim of all three projects is t...

Galileo L10 Satellites: Orbit, Clock and Signal-in-Space Performance Analysis

Sensors (Basel, Switzerland), 2021

The tenth launch (L10) of the European Global Navigation Satellite System Galileo filled in all orbital slots in the constellation. The launch carried four Galileo satellites and took place in July 2018. The satellites were declared operational in February 2019. In this study, we report on the performance of the Galileo L10 satellites in terms of orbital inclination and repeat period parameters, broadcast satellite clocks and signal in space (SiS) performance indicators. We used all available broadcast navigation data from the IGS consolidated navigation files. These satellites have not been reported in the previous studies. First, the orbital inclination (56.7±0.15°) and repeat period (50680.7±0.22 s) for all four satellites are within the nominal values. The data analysis reveals also 13.5-, 27-, 177- and 354-days periodic signals. Second, the broadcast satellite clocks show different correction magnitude due to different trends in the bias component. One clock switch and several ...

Galileo Constellation: Evaluation of Station Keeping Strategies

2009

Galileo is a Global Navigation System composed of 30 dedicated navigation satellites and a ground infrastructure with the main control centres in Europe and a network of dedicated stations deployed around the world. The purpose of this work is to analyse three Station Keeping (SK) Strategies for Galileo. All three strategies are based on the optimisation of biases for inclination, RAAN, semi-major axis and argument of latitude in order to minimize the number of manoeuvres, taking into account other operational considerations. A trade-off of the three Strategies will be presented in order to show the main advantages and the disadvantages of each of them, and the reasons to choose one of them for implementation in the Galileo System.

The DLR Project GalileoNAV: An Overview

In 2001 the DLR Institute of Communications and Navigation started an internal project called "GalileoNAV", which supports early work for the utilization, application and verification of Galileo. The project will last until 2006 and, therefore, is closely connected with the time schedule of the Galileo development and in-orbit-validation phases. The project consists of the following five main work packages: • Clock synchronization and time distribution, • Verification methods and algorithms, • Experimental verification systems, • Models and transmission methods, • Terminal development. This paper provides an overview about the structure and the main goals of the project and presents first results which have been obtained.