Europlanet Science Congress 2022
Palacio de Congresos de Granada, Spain
18 – 23 September 2022
Europlanet Science Congress 2022
Palacio de Congresos de Granada, Spain
18 September – 23 September 2022


Synergistic exploitation of small body missions in the 2020s 

The 2021 launches of the DART and Lucy spacecraft inaugurated a decade-long period of sustained mission flight rates to small bodies, with some fifteen individual spacecraft set to be dispatched to a diverse set of targets: near-Earth and main belt asteroids, cometary nuclei and comet-asteroid transition objects, Jupiter Trojans and small planetary moons.

This high flight rate implies concurrent operation of multiple spacecraft in-flight which, in turn, offers unprecedented opportunities for synergistic exploitation. For example, simultaneous observations of an asteroid or comet target from different vantage points across the solar system may be used to cross-verify instrument calibration, monitor for changes of the target and/or its environment over long time periods and expand observational coverage beyond the geometric and temporal constraints of any one mission.

In addition, new Earth-based and near-Earth survey facilities stand to complement the spacecraft investigations by allowing additional target characterisation and to apply the lessons learned from the targeted in situ studies at population level.

In this session we invite contributions focusing on such coordinated observations as to allow cross-calibration of spacecraft instruments, complement target characterisation efforts and for added science value. In this way, we hope to motivate the community to generate ideas for cross-project investigations. Flight projects relevant to this call include (but are not limited to) the DART, DESTINY+, Hayabusa II, HERA, Janus, Lucy, M-ARGO, Mars Moon eXplorer, NEA Scout, Psyche, Zheng-He and Comet Interceptor missions as well as Earth-based assets such as Gaia, JWST and the Rubin telescope. 

Co-organized by SB
Conveners: Apostolos Christou, Jamie Gilmour | Co-conveners: Josep Maria Trigo-Rodríguez, Paolo Tanga
| Fri, 23 Sep, 17:30–18:30 (CEST)|Room Andalucia 1
| Attendance Thu, 22 Sep, 18:45–20:15 (CEST) | Display Wed, 21 Sep, 14:00–Fri, 23 Sep, 16:00|Poster area Level 1

Session assets

Discussion on Slack

Orals: Fri, 23 Sep | Room Andalucia 1

Chairpersons: Apostolos Christou, Jamie Gilmour, Paolo Tanga
Luana Liberato, Paolo Tanga, David Mary, and Federica Spoto

(385186) 1994 AW1 was the first known asteroid with a satellite, discovered in 1994 using photometric lightcurve [1], the most successful technique used for this purpose. After that, more than 450 asteroids with satellites were discovered in the Solar System [2], almost 80% of them with orbits up to Jupiter, using many other observation techniques such as radar, and direct imaging from the ground and space. Recently in 2021, it was the first time that a stellar occultation provided the discovery of a companion asteroid by two independent events [3]. But still, a whole range of separation and size ratios is out of reach, where asteroids are too faint for high-resolution imaging, too far for radar, or do not provide a good signature in photometry. In that range, the use of highly accurate astrometry could be promising. In binary star research, companions are revealed by astrometry when the motion of a star around the common barycentre is measured (wobbling). The same approach becomes possible for asteroids, for the first time thanks to Gaia astrometry. As predicted way before the launch of the Gaia satellite[4], the high accuracy astrometric data could be used to find binary asteroids currently out of reach of detection. The Gaia mission provided to the scientific community astrometric solutions at an unprecedented precision [5]. Data Release 3 (DR3) provides new data for more than 150.000 asteroids, 10 times more than in Gaia DR2. Hence, using a large number of bodies in DR3 data with even better precision than in previous releases, we aim to search for astrometric asteroid binaries. Our approach starts by averaging the residuals to orbital fits over each transit in the focal plane. We select the asteroids with at least 10 values of residuals that are consecutive in time or anyway spanning a limited time range. This selection results in a sample of a bit more than 30000 objects. Then, using a Generalized Lomb-Scargle periodogram (see [6] and references therein), we run a period search on every sequence in order to find a signal that would represent the period and amplitude of the system's wobbling. The result is a map of the frequency power that indicates the goodness of data fitting. Since this technique always finds periodic fluctuations that could be spurious because of residual noise, we perform some statistical tests to determine the probability of fake detection and the relevance of the signal found. The first procedure is to run 10000 Monte Carlo simulations on white noise using the same time-sampling as the real data. The resulting p-value shows us how likely it is to obtain a peak as large as the largest peak found in the data if there was only noise in the data. The bodies that have a p-value smaller than 5% pass through the second calibration test. Again we perform 2000 MC simulations while adding white noise to the real data and checking how it affects the distribution of frequencies obtained from the GLS periodogram. If at least 10% of the distribution lies around the best frequency found for the real data, then we select this body. This procedure tells us the quality and confidence of the signal found, i.e., how easy it is to detect and how much we can trust that there is a signal in the data.  After the period search and statistical relevance tests, we obtain over 3300 candidates as possible binary asteroids. The last step is to check if the wobbling found is physically consistent. Hence we calculate the estimated range of density, separation and mass ratio for the binary candidates. We consider 7 g/cm3 as a maximum threshold for an acceptable maximum density.  In the end, we obtained almost 250 asteroid binary candidates that survived the 3-stage selection. We still can't guarantee that the periods found with such favourable conditions are caused by a companion satellite, but we show that there are some interesting pieces of evidence to support such a hypothesis. Further verification is required, both by statistical methods and observations, to validate our findings.



[1] Pravec, P. & Hahn, G. 1997, Icarus, 127, 431

[2] Johnston, Wm. Robert. "Asteroids with Satellites Database" May 16, 2022. Johnston's Archive

[3] Gault D., Nosworthy P., Nolthenius R., Bender K., Herald D., 2022, MPBu, 49, 3

[4] Tanga, P., Hestroffer, D., Delbò, M., et al. 2008, Planetary and Space Science, 56, 1812

[5] Gaia Collaboration, Spoto, F., Tanga, P., et al. 2018b, Astronomy and Astrophysics, 616, A13

[6] VanderPlas, J. 2018, ApJS, 236, 16

[7] Hestroffer, D., Dell’Oro, A., Cellino, A., & Tanga, P. 2010, in Lecture Notes in Physics, Berlin Springer Verlag, Vol. 790, 251–340



This work presents results from the European Space Agency (ESA) space mission Gaia. Gaia data are being processed by the Gaia Data Processing and Analysis Consortium (DPAC). Funding for the DPAC is provided by national institutions, in particular the institutions participating in the Gaia MultiLateral Agreement (MLA). The Gaia mission website is The Gaia archive website is

This study was financed in part by the Coordenação de Aperfeiçoamento de Pessoal de Nível Superior – Brasil (CAPES) – Finance Code 001, also by CAPES-PRINT Process 88887.570251/2020-00, by the French Programme National de Planetologie, and by the BQR program of Observatoire de la Côte d'Azur. 

How to cite: Liberato, L., Tanga, P., Mary, D., and Spoto, F.: Satellite Search in Gaia DR3 astrometry, Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-630,, 2022.

Geraint Jones, Colin Snodgrass, and Cecilia Tubiana and the The Comet Interceptor Consortium

In 2019, Comet Interceptor was selected by the European Space Agency, ESA, as the first in its new class of F missions. At the time of this writing, formal adoption of the mission is anticipated for early June 2022. The Japanese space agency, JAXA, is making a major contribution to the project. Comet Interceptor's primary science goal is to characterise for the first time, a yet-to-be-discovered long-period comet, preferably dynamically new, or an interstellar object. An encounter with a comet approaching the Sun for the first time will provide valuable data to complement information gathered by all previous comet missions, which through necessity all visited more evolved short period comets. The spacecraft will be launched in 2029 with the Ariel mission to the Sun-Earth Lagrange Point, L2. This relatively stable location allows a rapid response to the appearance of a suitable target comet, which will need to cross the ecliptic plane through an annulus centered on the Sun that contains Earth’s orbit. A suitable new comet would be searched for from Earth, with short period comets acting as mission backup targets. Powerful facilities such as the Vera Rubin Observatory make finding a suitable comet nearing the Sun very promising, and the spacecraft could encounter an interstellar object if one is found on a suitable trajectory. The spacecraft must cope with a wide range of target activity levels, flyby speeds, and encounter geometries. This flexibility has significant impacts on the spacecraft solar power input, thermal design, and shielding that can cope with dust impacts. Comet Interceptor comprises a main spacecraft and two probes, one provided by ESA, the other by JAXA, which will be released by the main spacecraft on approach to the target. The main spacecraft, which would act as the primary communication point for the whole constellation, would be targeted to pass outside the hazardous inner coma, making remote and in situ observations on the comet’s sunward side. Planned measurements of the target include its surface composition, shape, and structure, its dust environment, and the gas coma’s composition. A unique, multi-point ‘snapshot’ of the comet- solar wind interaction region will be obtained, complementing single spacecraft observations at other comets. We shall describe the science drivers, planned observations, and the mission’s instrument complement, to be provided by consortia of institutions in Europe and Japan.

How to cite: Jones, G., Snodgrass, C., and Tubiana, C. and the The Comet Interceptor Consortium: The Comet Interceptor Mission, Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-1085,, 2022.

The Twinkle Space Mission's Solar System Survey
Billy Edwards, Ben Wilcock, Max Joshua, Ian Stotesbury, Marcell Tessenyi, Richard Archer, and Yoga Barrathwaj Raman Mohan
Ana-Maria Piso-Grigore, Angelo Voicu, Pierre Sprimont, Bogdan Bija, Oscar Alonso-Lasheras, and Vlad Olteanu

Space Surveillance and Tracking (SST) requires the development of observational campaigns to early identify Earth orbiting objects, estimate their orbital elements and monitor the evolution of their trajectories.

With a growing number of satellites being launched every year, there is an increasing interest in SST at worldwide level and especially across the EU. In this context, Romania is one of the few EU member states involved in such activities.

SST systems must implement an Image Data Reduction Subsystem, able to timely process the continuous exposures taken in an automatic and continuous way by optical telescopes, analyse these data sets to identify objects of interest (target objects) and retrieve accurate measurements of the apparent position and brightness of the detected objects. In the last step, the tool generates tracklet information for the identified target objects.

In this context, The Generic Data Reduction Framework for Space Surveillance -  gendared, prototyped initially by GMV in the frame of an ESA Romanian Industry Incentive Scheme project, is intended to be used in order to support the operational reduction of the image data acquired by optical telescopes. gendared receives as input the raw images taken by the telescope, and generates as output astrometric and photometric data for the target objects detected in the observation images.

The key aspects that drove the development of gendared and its advantages include the fact that the software is autonomous and unassisted, can process images in near real-time, can cope with different image acquisition schemas, and is configurable and modular.

As of the end of the prototyping phase and the acceptance of the software by ESA, gendared has been successfully tested and validated on Romanian telescopes and developed further for various operational use cases of different telescopes, such as the German Aerospace Centre (DLR) telescopes.

Furthermore, since mid-2020, gendared is part of a larger architecture of GMV products supporting the operational data processing activities in Romanian Space Agency’s SST Operational Centre (COSST), which ensures the Romanian contribution to the EUSST Consortium. In this case gendared is covering, in a centralized architecture, the processing of the data coming from the Romanian optical telescopes involved in EUSST. The software was further upgraded for this purpose, with new algorithms and processing pipelines included.

Most recently GMV has also won a Romanian Research & Development grant to upgrade gendared with artificial intelligence algorithms. This project involves a consortium led by GMV, with the Faculty of Automatic Control and Computer Science and the Astronomical Institute of the Romanian Academy as partners. By integrating artificial intelligence techniques into the current gendared framework, we aim to improve its performance, reduce user involvement and computational costs, as well as increase pipeline autonomy. The upgraded solution will be tested and validated in representative scenarios based on real telescope data, with the ultimate goal of converting the prototype into a product that will be validated in an SST operational environment on a wide range of telescopes.



How to cite: Piso-Grigore, A.-M., Voicu, A., Sprimont, P., Bija, B., Alonso-Lasheras, O., and Olteanu, V.: gendared: the Generic Data Reduction Framework for Space Surveillance, Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-35,, 2022.

Display time: Wed, 21 Sep 14:00–Fri, 23 Sep 16:00

Posters: Thu, 22 Sep, 18:45–20:15 | Poster area Level 1

Chairpersons: Apostolos Christou, Jamie Gilmour, Paolo Tanga
Anamarija Stankov, Francesco Ratti, Nicola Rando, Michael Kueppers, Carlos Corral Van Damme, Arno Wielders, Kristin Wirth, Virginie Agnolon, and Joel Asquier

The Comet Interceptor mission was selected by ESA in 2019 as the first fast class science mission, to be launched in 2029. As an F-class mission, Comet-I has a reduced definition and implementation time compared to medium or large class mission and strict limits regarding resources and cost. For example, the time between mission proposal selection and delivery of the flight models of the instruments, is about 5-6 years, precluding the possibility of new technology developments. This fast and resource constrained mission development presents unique challenges for the platform as well as for the payload.

The mission’s main science goal is to characterise a dynamically new comet, or a new interstellar object, using multi-point observations, performed by the instruments on board the main spacecraft A and its two probes, B1 and B2. Probe B1 will be provided by JAXA and probe B2 will be provided by ESA.  

Comet Interceptor will be launched with an Ariane launcher, together with ESA’s ARIEL satellite, to the Sun-Earth L2 point. There the satellite will remain in a waiting position until it continues its journey to a newly detected comet or interstellar body. Comet-I will perform a close fly-by of this object and will also release two small probes, B1 and B2, which will observe the object from a much closer distance than spacecraft A. The satellite is designed for a total mission lifetime of 6 years with a science operations phase of up to 6 months after the closest encounter at fly-by.

In Figure 1 we show the main mission phases: Launch, transfer to L2, waiting position at L2, transfer to the target, and fly-by:

Figure 1: Comet Interceptor mission phases.


In this poster we describe the Comet Interceptor mission, the scientific payload on the two ESA elements, and its accommodation on spacecraft A and probe B1.

The scientific payload on the spacecraft A comprises:

  • CoCa - camera for high resolution colour imaging of the target’s surface and inner coma.
  • MANIaC – mass spectrometer based on the time-of flight principle, measuring in situ volatiles’ total and relative abundances in the coma.
  • MIRMIS - mapping the ice and mineral composition of the target nucleus and coma and the surface temperature of the nucleus
  • DFP-A: Dust, Fields, and Particles suite: three particle detectors measuring electrons, ions and energetic neutral atoms, as well as a dust detector and a magnetometer - to detect and measure charged gases, energetic neutral atoms, dust, and magnetic fields surrounding the comet.

The scientific payload on the probe B2 comprises:

  • OPIC - imager for mapping of the nucleus and its dust jets.
  • EnVisS - to map the entire sky within the comet's head and near-tail, to reveal changing structures within the dust, neutral gas, and ionized gases.
  • DFP-B: Dust, Fields, and Particles suite (subset of DFP-A sensors) -  the dust detector, and magnetometer.

How to cite: Stankov, A., Ratti, F., Rando, N., Kueppers, M., Corral Van Damme, C., Wielders, A., Wirth, K., Agnolon, V., and Asquier, J.: The ESA Comet Interceptor mission and its payload complement, Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-523,, 2022.