ISSN: 2168-9792
+44-77-2385-9429
Davide Vignotto
University of Trento, Italy
Scientific Tracks Abstracts: J Aeronaut Aerospace Eng
LISA Pathfinder (LPF) is an ESA (European Space Agency) mission aimed at testing new technologies in the field of
gravitational waves detection. The LPF scientific payload, the LISA Technology Package (LTP), contains two test masses
(TMs) that must be set into free-fall inside their Gravitational Reference Sensors (GRS) with a minimum acceleration noise
level, in order to provide the sensing bodies for the detection of gravitational waves. Driven by this requirement, the GRS design
minimizes noisy forces by means of a strict control of the force budget and the adoption of large gaps between the TM and its
electrode housing (EH). This however calls for a mechanism to secure the TM during the spacecraft launch and to release it
to free fall for the science phase. The release maneuver is mission-critical and is performed by the grabbing positioning and
release mechanism (GPRM), composed of two identical and opposed units which engage the TM by means of two plungers and
release-dedicated tips. After a successful nominal and extended mission (2016-2017), due to its criticality for future missions
(e.g. LISA), the GPRM release function has been intensively tested. The release performance of the GPRM can be estimated
by the TM residual velocity after the disengagement, which should be minimal in order to allow the subsequent capture on
behalf of the electrostatic actuation system. However, significant deviations occurred with respect to such a baseline, produced
by unexpected configurations of the GPRM-TM system. The dedicated in-flight test campaign made it possible to understand
some phenomena which produced such a behavior and formulate some risk-reduction strategies. In this work, the releases
performed by the GPRM have been analyzed, focusing mainly on two aspects: i) studying the mechanical configuration of the
system in pre-release phases and ii) evaluating the residual velocity of the TM after each release.
Recent Publications
1. D Bortoluzzi et al. (2010) Object injection in geodesic conditions: in-flight and on-ground testing issues. Adv. Space Res.
45(11):1358-1379.
2. D Bortoluzzi et al. (2011) Measurement of momentum transfer due to adhesive forces: on-ground testing of in-space
body injection into geodesic motion. Rev. Sci. Instrum. 82(12):125107.
3. D Bortoluzzi et al. (2009) LISA Pathfinder test mass injection in geodesic motion: status of the on-ground testing. Class.
Quant. Grav. 26(9).1-11.
4. C Zanoni and D Bortoluzzi (2015) Experimental-analytical qualification of a piezoelectric mechanism for a critical space
application. IEEE/ASME Transactions on Mechatronics. 20(1):427-437.
5. D Bortoluzzi, C. Zanoni and J W Conklin (2017) On-ground testing of the role of adhesion in the LISA- Pathfinder test
mass injection phase. Advances in Space Research. 59(10):2572-2582.
Davide Vignotto is a PhD student at the University of Trento, Italy, where he graduated in Mechatronics Engineering. His master’s thesis focuses on the test mass release dynamics of the space mission LISA Pathfinder. He is interested in systems modelling and identification in the aerospace field. His research interest include: data analysis and systems identification.