Prepared by: MORE Team MORE Relativity Meeting February 16-17, 2009 Rome Simulation of the solar conjunction experiment with BepiColombo.

Slides:



Advertisements
Similar presentations
Accurate light-time correction due to a gravitating mass A mathematical follow-up to Cassinis experiment Bruno Bertotti Dipartimento di Fisica Nucleare.
Advertisements

AOGS Singapore June 2005 Paper ID: 58-PS-A0321 BepiColombo – Mission to Mercury Mission Overview Rita Schulz Johannes.
March , Birmingham GR tests and micro-arcsecond light bending parameters by global and differential Gaia mesurements Maria Teresa Crosta Astronomical.
1 Measurement of the Gravitational Time Delay Using Drag-Free Spacecraft and an Optical Clock Neil Ashby, Dept. of Physics, UCB 390, University of Colorado,
Maxwell’s Equations and Electromagnetic Waves
U N C L A S S I F I E D Operated by the Los Alamos National Security, LLC for the DOE/NNSA Pitch angle evolution of energetic electrons at geosynchronous.
“PLANET AND GALAXY WE LIVE…” Presentation M. Filonenko K. Tusov School 1173, Form 9E GUIDANCE – Markova S.A.
Physics 1.2.
Prepared by: M. Marabucci, L. Iess M. Di Benedetto, S. Finocchiaro, A.Genova, R. Meriggiola, P. Racioppa, G.Rapino Progress Meeting 15 October 2009 Simulations.
Precision versus Accuracy (1) Precision is the variation of X around – expressed as standard deviation or variance Accuracy is the closeness of to the.
Titan’s Thermospheric Response to Various Plasma Environments Joseph H. Westlake Doctoral Candidate The University of Texas at San Antonio Southwest Research.
Experimental investigations of the flow during the stage separation of a space transportation system Andrew Hay Aerospace Engineering with German.
FIREBIRD Ian Lyon Engineering and Physics Carroll College Simulation of the Precise Separation of a Two-Nanosatellite System using Differential Drag.
Pioneer Anomaly Test – Jonathan Fitt 1 System Design Assessment for a Mission to Explore the Pioneer Anomaly Jonathan Fitt Monday, 15 June 2015
Observations of Open and Closed Magnetic Field Lines at Mars: Implications for the Upper Atmosphere D.A. Brain, D.L. Mitchell, R. Lillis, R. Lin UC Berkeley.
Page 1 1 of 20, EGU General Assembly, Apr 21, 2009 Vijay Natraj (Caltech), Hartmut Bösch (University of Leicester), Rob Spurr (RT Solutions), Yuk Yung.
INSTITUTO DE SISTEMAS E ROBÓTICA 1/31 Optimal Trajectory Planning of Formation Flying Spacecraft Dan Dumitriu Formation Estimation Methodologies for Distributed.
Lunar CRater Observation and Sensing Satellite Project LCROSS Site Selection Workshop Oct , 2006 NASA/ARC, Mountain View, California LCROSS Orbital.
On the Accuracy of Modal Parameters Identified from Exponentially Windowed, Noise Contaminated Impulse Responses for a System with a Large Range of Decay.
An active Seismic experiment on Bepi-Colombo Lognonné, P, Garcia. R (IPGP, France) P.; Gudkova, T.(IPE, Russia) ; Giardini, D., Lombardi D. (ETHZ, Switzerland);
Modern Navigation Thomas Herring MW 11:00-12:30 Room
Acceleration - rate of change of velocity (speed or direction), occurs any time an unbalanced force is applied.
SACE Stage 2 Physics Motion in 2 Dimensions.
Thursday, October 11 Journal: Define gravity and inertia. Schedule: Gravity Notes Gravity Video Homework: None.
System Design Assessment for a Mission to Explore the Pioneer Anomaly Jonathan Fitt School of Physics and Astronomy, University of Birmingham, Edgbaston,
Effects of ionospheric small- scale structures on GNSS G. WAUTELET Royal Meteorological Institute of Belgium Ionospheric Radio Systems & Techniques (IRST)
Maria Teresa Crosta and Francois Mignard Small field relativistic experiment with Gaia: detection of the quadrupolar light deflection.
Kepler’s first law of planetary motion says that the paths of the planets are A. Parabolas B. Hyperbolas C. Ellipses D. Circles Ans: C.
Polar Topographic Knowledge Prior to LCROSS Impact David E. Smith 1, Maria T. Zuber 2 1 NASA/Goddard Space Flight Center 2 Massachusetts Institute of Technology.
Recent determination of Gamma with Cassini M.T. Crosta, F. Mignard CNRS-O.C.A. 5th RRFWG, June, Estec.
Ultimate Spectrum of Solar/Stellar Cosmic Rays Alexei Struminsky Space Research Institute, Moscow, Russia.
Chapter 22 Planet Earth.
1 POS MV Vertical Positioning March Where we fit in! “Other sensors (notably modern heave-pitch-roll sensors) can contribute to achieving such.
Universal Gravitation.
Modeling the upper ocean response to Hurricane Igor Zhimin Ma 1, Guoqi Han 2, Brad deYoung 1 1 Memorial University 2 Fisheries and Oceans Canada.
Bone Trajectories and Model Simulations Kathleen Mandt, Ray Goldstein, Christoph Koenders May 29, 2013 IES Team Meeting – San Antonio.
FAST LOW THRUST TRAJECTORIES FOR THE EXPLORATION OF THE SOLAR SYSTEM
ADCS Review – Attitude Determination Prof. Der-Ming Ma, Ph.D. Dept. of Aerospace Engineering Tamkang University.
Chapter 6 Gravitation and Newton’s Synthesis HW5: Chapt 6: Pb. 11, Pb. 24, Pb. 25 and Chapt. 7: Pb 6, Pb.11, Pb. 16, Pb.19, Pb. 21 –Due Friday, Oct. 9.
Chapter 3: Maximum-Likelihood Parameter Estimation l Introduction l Maximum-Likelihood Estimation l Multivariate Case: unknown , known  l Univariate.
Effective drift velocity and initiation times of interplanetary type-III radio bursts Dennis K. Haggerty and Edmond C. Roelof The Johns Hopkins University.
Issue/Revision: 1.0 Reference: Status: For information Only ESA UNCLASSIFIED - For Official Use Solar Orbiter: Launch Options Favouring Data.
also known as “Luna” in Latin it orbits around the Earth at an angle of inclination of 5.14° from the ecliptic plane.
TIDES. Tides  Tides are long period waves that move in the ocean in response to the gravitational force of the sun and the moon.  Tides originate in.
West Hills College Farm of the Future. West Hills College Farm of the Future Precision Agriculture – Lesson 2 What is GPS? Global Positioning System Operated.
Chapter 2 GPS Crop Science 6 Fall 2004 October 22, 2004.
Analysis of Nonlinearity Correction for CrIS SDR April 25, 2012 Chunming Wang NGAS Comparisons Between V32 and V33 Engineering Packets.
EUM/OPS/VWG/11 Issue /06/2011 Yoke Yoon Yago Andres Christian Marquardt COSMIC GPS Data Processing Slide: 1.
Parameters : Temperature profile Bulk iron and olivine weight fraction Pressure gradient. Modeling of the Martian mantle Recently taken into account :
LLR Analysis – Relativistic Model and Tests of Gravitational Physics James G. Williams Dale H. Boggs Slava G. Turyshev Jet Propulsion Laboratory California.
Newton’s Law of Universal Gravitation:
Introduction to Earth Science : EARTH SCIENCE: Chapter 1.
Unit 2- Force and Motion Vocabulary- Part I. Frame of Reference  A system of objects that are not moving with respect to each other.
Some problems in the optimization of the LISA orbits Guangyu Li 1 , Zhaohua Yi 1,2 , Yan Xia 1 Gerhard Heinzel 3 Oliver Jennrich 4 1 、 Purple Mountain.
A Closer Look at Damaging Surface Winds Timothy A. Coleman and Kevin R. Knupp The University of Alabama in Huntsville AMS 12th Conference on Mesoscale.
Formosat-3/COSMIC WorkshopNov 28 - Dec 1, 2006Taipei, Taiwan Estimates of the precision of LEO orbit determination and GPS radio occultations from the.
1 Pruning of Ensemble CME modeling using Interplanetary Scintillation and Heliospheric Imager Observations A. Taktakishvili, M. L. Mays, L. Rastaetter,
Investigations on (radial) offsets between different Swarm orbit solutions 8 September th Swarm Data Quality Workshop, IPGP, Paris Heike Peter (PosiTim),
Frames of Reference.  Displacement is a _______________ line distance between where something ______________ and where it ends.  Average velocity is.
PRESENTATION OUTLINE Experiment Objective Introduction Data Conclusion Recommendations.
Lunar CRater Observation and Sensing Satellite Project LCROSS Astronomer Workshop Feb. 29, 2008 NASA/ARC, Mountain View, California Mission Design & Observation.
A Parametric Study of Interplanetary Mission Using Solar Sail
Space Geodesy Branch Highlights, August 2002 CONT02 VLBI Campaign
Mac Keiser and Alex Silbergleit
Flight Dynamics Michael Mesarch Frank Vaughn Marco Concha 08/19/99
Sun – Earth Survey answers and explanations
Dynamics and Control Attitude dynamics Communications Pointing
Mac Keiser and Alex Silbergleit
Orbits and How They Work
LIP Lisbon We would sugest to include in the Statement of Work the following points: The development of an engineering tool to extrapolate measured solar.
Presentation transcript:

Prepared by: MORE Team MORE Relativity Meeting February 16-17, 2009 Rome Simulation of the solar conjunction experiment with BepiColombo

MORE Relativity Meeting, February , Rome Introduction being r 1 and r 2, respectively, the Sun-S/C and Sun-Earth distances, and b the impact parameter. A solar conjunction experiment in cruise is foreseen for April In principle, the accuracy of the measurement of the post-Newtonian parameter γ should be higher in cruise rather than in orbit, due to the absence of gravity gradient An electromagnetic wave passing near the Sun is affected by a relativistic delay, expressed as:

MORE Relativity Meeting, February , Rome Goals of the simulation Goals:  Simulating the solar conjunction experiment occurring in 2016; a best case will be presented (upper limit to the accuracy in the estimation of γ);  Comparing the results to what we can achieve doing the experiment in 2017;  Determining the effect of uncalibrated non-gravitational acceleration noise on the measurement. S/C SEP Geometry: b Sun Earth

MORE Relativity Meeting, February , Rome Relativistic delay variation Sun–Earth–Probe angle variation Relativistic delay variation

MORE Relativity Meeting, February , Rome Simulation setup Dynamic model:  Model for solar pressure: flat plate of 55 m 2 area, average thermo-optical coefficients, always pointing toward the Sun (in order to maintain a constant sun-aspect-angle)  Absence of orbital and attitude maneuvers Observables:  Observables: range, one measurement every 20 sec (the range rate does not give a significant contribution), for 20 days  Two DSN stations, providing a coverage of 15 hours per day  Observables under 8 solar radii have not been considered  Gaussian noise added (we have supposed to cancel the plasma noise, by using the multi-frequency link), with a standard deviation of 20 cm

MORE Relativity Meeting, February , Rome Estimation Estimation:  Estimation of the state vector of BepiColombo and γ  The starting value of γ has been set to that obtained with the Cassini mission γ = 1 + (2.1 ± 2.3)x10 -5 γ = 1 – (8.5 ± 8.7)x10 -6 Above the goal of the experiment!

MORE Relativity Meeting, February , Rome Estimation γ = 1 + (1.5 ± 2.6)x10 -6 Compatible with the goal of the experiment

MORE Relativity Meeting, February , Rome Conclusions In conclusion:  The geometry of the solar conjunction in 2016 seems not to meet the scientific objective of MORE. In particular, the accuracy is more than 3 times worse wrt what we would like to achieve;  On the contrary, the solar conjunction in 2017 could allow a very precise measurement.