Autonomous close-proximity operations in space: The PRoBa-3 rendezvous experiment (P3RVX)

Research output: Chapter in Book/Report/Conference proceedingArticle in proceedings – Annual report year: 2019Researchpeer-review

  • Author: Rosa, Paulo

    Elecnor DEIMOS, Portugal

  • Author: Silva, Pedro Freire

    Elecnor DEIMOS, Portugal

  • Author: Parreira, Baltazar

    Elecnor DEIMOS, Portugal

  • Author: Hagenfeldt, Miguel

    Elecnor DEIMOS, Portugal

  • Author: Fabrizi, Andrea

    Elecnor DEIMOS, Portugal

  • Author: Pagano, Antonio

    Elecnor DEIMOS, Portugal

  • Author: Russo, Antonio

    Elecnor DEIMOS, Portugal

  • Author: Salvi, Samuele

    Elecnor DEIMOS, Portugal

  • Author: Kerr, Murray

    Elecnor DEIMOS, Portugal

  • Author: Radu, Silvana

    Institute of Space Sciences, Romania

  • Author: Daoud-Moraru, Anthonius

    Institute for Space Sciences, Bucharest, Romania

  • Author: Pandele, Constantin Alexandru

    Institute for Space Sciences, Bucharest, Romania

  • Author: Stoica, Adrian Mihail

    University Politehnica of Bucharest, Romania

  • Author: Mihai, Sergiu Stefan

    University Politehnica of Bucharest, Romania

  • Author: Pedersen, David A. K.

    Measurement and Instrumentation Systems, National Space Institute, Technical University of Denmark, Elektrovej, 2800, Kgs. Lyngby, Denmark

  • Author: Jørgensen, John Leif

    Measurement and Instrumentation Systems, National Space Institute, Technical University of Denmark, Elektrovej, 2800, Kgs. Lyngby, Denmark

  • Author: Riveras, Sergio Tiraplegui

    SENER Ingenieria y Sistemas, Spain

  • Author: Contreras, Rafael

    SENER Ingenieria y Sistemas, Spain

  • Author: Cropp, Alexander

    ESTEC, Netherlands

  • Author: Grzymisch, Jonathan

    ESTEC, Netherlands

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Proba-3 is a Formation Flying (FF) technology demonstration mission from ESA. The main mission, covers the design, development, and in-fight operation of two small satellites, for the full-scale test and validation of FF mission architectures and techniques. Proba-3 has just finished the design phase and it is now starting the manufacturing and verification phase D aiming at launch before beginning of the next decade. The Proba-3 mission also offers a unique opportunity to test other technologies, including to perform Relative Dynamics Experiments (RDE). The Proba-3 RendezVous eXperiment (P3RVX) takes advantage of this opportunity to exploit the suitability of Proba-3 for the maturation of RV technology, in particular with non-cooperative targets, with two satellites, in a highly elliptical orbit (perigee and apogee height of 600 and 60,530 km, respectively), using optical Navigation. The P3RVX consortium is led by DEIMOS and includes the Technical University of Denmark (DTU) and University Politehnica of Bucharest/Institute of Space Sciences (UPB/ISS). This paper provides an overview of the P3RVX, which aims to perform in-orbit demonstrations of the Guidance, Navigation, and Control (GNC) subsystem (including the Fault Detection, Isolation, and Recovery (FDIR) functions), the operations, the autonomy approach, and the Verification and Validation (VV), for missions in highly-elliptical orbits with fast and time-varying dynamics. This includes, in addition, the in-flight testing of DTU's Vision Based System (VBS) software for non-cooperative scenarios. Typical close-proximity operations are considered, including non-cooperative rendezvous and forced-motion (inspection, approach/retreat, and station-keeping) maneuvers during perigee, with the latter being performed both in eclipse and in Sun-illuminated conditions. These high-level mission requirements are translated into the design of trajectories satisfying a number of constraints. In-house-developed tools are adopted to solve this problem, ensuring that the trajectories are passively safe - whenever possible - in case of an inhibiting failure. Moreover, trajectory design is required to consider the limitations of actuators, as well as sensors. The outcomes of P3RVX are aligned with ESA technology lines and, as such, are expected to have a significant impact on the community. In particular, in-orbit demonstration of autonomous GNC for elliptical orbits (in both fast and slow dynamic regions) and autonomous non-cooperative close-proximity GNC using a camera; provide technology developments generally applicable to future programs; and a significant maturation of these technologies, needed to support short- and medium-term Clean Space and ADR lines, as well as the development of Space Service Vehicles (SSVs).
Original languageEnglish
Title of host publicationProceedings of the 69th International Astronautical Congress: Involving Everyone
Number of pages13
Volume2018
PublisherInternational Astronautical Federation
Publication date2018
Article numberIAC-18-C1.5.10
ISBN (Electronic)9781510881655
Publication statusPublished - 2018
Event69th International Astronautical Congress (IAC 2018) - Bremen, Germany
Duration: 1 Oct 20185 Oct 2018

Conference

Conference69th International Astronautical Congress (IAC 2018)
CountryGermany
CityBremen
Period01/10/201805/10/2018
SeriesProceedings of the International Astronautical Congress, Iac
ISSN0074-1795

    Research areas

  • GNC, Proba-3, Rendezvous, Vision-based systems
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