A dataset provided by the European Space Agency

DOI 10.5270/esa-qxiz7d6
Abstract This archive contains ancillary data for the comet phase of the ROSETTA Lander. It contains information on the trajectory, attitude, position of the Lander and on the Sun directions. The data has been taken around the time of the landing on 67P. The data set has been created from the CONSERT, ROLIS, ROMAP, RSI and OSIRIS data. V2.0 provides improvement of the trajectories and attitude files and in the latest position of the lander.
Description This data set contains ancillary information for the Rosetta Lander, namely trajectory, attitude, position and Sun directions. The data were generated by the CNES/SONC-FD team. The data concern three different phases of the Philae mission 1) SDL (Separation Descent Landing), the descent ranging from the release of Philae to the first touchdown 2) RBD (Rebounds), the rebound ranging from first touchdown to final landing. 3) FSS (First Science Sequence), the rest on the final landing site. To generate this data set the data of the following instruments have been used: CONSERT, ROMAP, ROLIS, RSI and OSIRIS. The Lander trajectory, sun direction are provided by SONC FD team using RMOC (comet ephemeris an rotation) data, gravity model from GRGS (Groupe de Recherche de Geodesie Spatiale), shape models from OSIRIS. The Lander attitude is derived from ROMAP data. All files are .ROS or .TXT files. The V2.0 provides: - updates of the RBD spice kernel trajectories - correction of FSS attitude of the Lander - addition of LATT in SDL in Orbiter frame - improvement of BSP files - latest Lander position after finding the Lander in Sept 2016. All the improvement related to the SPICE kernels are described in DOCUMENT/SPICE_UPDATES.PDF. DOCUMENT/V2_UPDATES.TXT summarises the list of all improvements.
Temporal Coverage 2014-01-21T05:01:37Z/2015-01-01T00:00:00Z
Version V2.0
Mission Description TABLE OF CONTENTS ---------------------------------- = ROSETTA Mission Overview = ROSETTA Mission Objectives - Science Objectives = Mission Profile = Mission Phases Overview - Mission Phase Schedule - Solar Conjunctions/Oppositions - Payload Checkouts = Mission Phases Description - Launch phase (LEOP) - Commissioning phase - Cruise phase 1 - Earth swing-by 1 - Cruise phase 2 (and Deep Impact) - Mars swing-by - Cruise phase 3 - Earth swing-by 2 - Cruise phase 4 (splitted in 4-1 and 4-2) - Steins flyby - Earth swing-by 3 - Cruise phase 5 - Lutetia flyby - Rendez-Vous Manouver 1 - Cruise phase 6 - Rendez-Vous Manouver 2 - Near comet drift (NCD) phase - Approach phase - Lander delivery and relay phase - Escort phase - Near perihelion phase - Extended mission = Orbiter Experiments - ALICE - CONSERT - COSIMA - GIADA - MIDAS - MIRO - OSIRIS - ROSINA - RPC - RSI - VIRTIS - SREM = LANDER (PHILAE) - Science Objectives - Lander Experiments = Ground Segment - Rosetta Ground Segment - Rosetta Science Operations Center - Rosetta Mission Operations Center - Rosetta Lander Ground Segment - Lander Control Center - Science Operations and Navigation Center - Rosetta Scientific Data Archive = Acronyms ROSETTA Mission Overview = The ROSETTA mission is an interplanetary mission whose main objectives are the rendezvous and in-situ measurements of the comet 67P/Churyumov-Gerasimenko, scheduled for 2014/2015. The spacecraft carries a Rosetta Lander, named Philae, to the nucleus and deploys it onto its surface. A brief description of the mission and its objectives can be found in [GLASSMEIERETAL2007A]. A detailed description of the mission analysis can be found in the ROSETTA User Manual [RO-DSS-MA-1001], and the flight Operations Plan [RO-ESC-PL-5000]. On its long way to the comet nucleus after a Launch by Ariane 5 P1+ in March 2004, the ROSETTA spacecraft orbited the Sun fo...
Date Published 2018-04-15T00:00:00Z
Publisher And Registrant European Space Agency
Credit Guidelines European Space Agency, 2018-04-15T00:00:00Z, RL-C-MULTI-5-ANCDR, V2.0. https://doi.org/10.5270/esa-qxiz7d6