IMF derivation from Pickup Ions observed by ASPERA 3 2005-4-27 1331-1344 UT 2005-7-12 1133-1146 UT 2005-6-3 0602-0615 UT M. Yamauchi B ion ion motion in.

Slides:



Advertisements
Similar presentations
Lecture 5: Constraints I
Advertisements

The Quantum Mechanics of Simple Systems
PHYS 218 sec Review Chap. 3 Motion in 2 or 3 dimensions.
Foreshock studies by MEX and VEX FAB: field-aligned beam FAB + FS: foreshock M. Yamauchi et al.
1 Projectile motion an object dropped from rest an object which is thrown vertically upwards an object is which thrown upwards at an angle A projectile.
PRECIPITATION OF HIGH-ENERGY PROTONS AND HYDROGEN ATOMS INTO THE UPPER ATMOSPHERES OF MARS AND VENUS Valery I. Shematovich Institute of Astronomy, Russian.
Martian Pick-up Ions (and foreshock): Solar-Cycle and Seasonal Variation M. Yamauchi(1); T. Hara(2); R. Lundin(3); E. Dubinin(4); A. Fedorov(5); R.A. Frahm(6);
Copyright © 2009 Pearson Education, Inc. Force on an Electric Charge Moving in a Magnetic Field.
DS-1/Plasma Experiment for Planetary Exploration (PEPE) PEPE – is a particle spectrometer capable of resolving energy, angle and mass & charge composition.
Expected Influence of Crustal Magnetic Fields on ASPERA-3 ELS Observations: Insight from MGS D.A. Brain, J.G. Luhmann, D.L. Mitchell, R.P. Lin UC Berkeley.
Lecture III Curvilinear Motion.
Relative Motion. Point of View  A plane flies at a speed of 200. km/h relative to still air. There is an 80. km/h wind from the southwest (heading 45°
Lecture III Curvilinear Motion.
Physics 211 Space - time & space-space diagrams Kinetic Equations of Motion Projectile motion Uniform circular motion Moving coordinate systems Relative.
March 2, 2011 Fill in derivation from last lecture Polarization of Thomson Scattering No class Friday, March 11.
Copyright © 2009 Pearson Education, Inc. Lecture 8 - Magnetism.
Ch 3.9: Forced Vibrations We continue the discussion of the last section, and now consider the presence of a periodic external force:
The Hydrogen Atom Quantum Physics 2002 Recommended Reading: Harris Chapter 6, Sections 3,4 Spherical coordinate system The Coulomb Potential Angular Momentum.
KINEMATICS OF PARTICLES PLANE CURVILINEAR MOTION
Colorado Center for Astrodynamics Research The University of Colorado 1 STATISTICAL ORBIT DETERMINATION Satellite Tracking Example of SNC and DMC ASEN.
Chang-Kui Duan, Institute of Modern Physics, CUPT 1 Harmonic oscillator and coherent states Reading materials: 1.Chapter 7 of Shankar’s PQM.
Periodic Motion - 1.
IMF direction derived from cycloid-like ion distributions observed by Mars Express M. Yamauchi, Y. Futaana, R. Lundin, S. Barabash, M. Holmström (IRF-Kiruna,
Finite Gyroradius Effect in Space and Laboratory 1. Radiation belt (Ring current) 2. Auroral phenomena (Substorm current) 3. Shock acceleration and upstream.
Projectile Motion Projectiles launched at an angle.
Normalisation modelling sources Geant4 tutorial Paris, 4-8 June 2007 Giovanni Santin ESA / ESTEC Rhea System SA.
Chapter 4 Motion in Two Dimensions. Kinematics in Two Dimensions Will study the vector nature of position, velocity and acceleration in greater detail.
Circular Motion Topics Angular Measure Angular Speed and Velocity Uniform Circular Motion and Centripetal Acceleration Angular Acceleration.
Foreshock studies by MEX and VEX FAB: field-aligned beam FAB + FS: foreshock M. Yamauchi et al.
Introduction to Space Weather Jie Zhang CSI 662 / PHYS 660 Spring, 2012 Copyright © The Heliosphere: The Solar Wind March 01, 2012.
Sect 5.7: Heavy Symmetrical Top with 1 Point Fixed, Part I Euler’s Eqtns of Motion for a Rigid Body with 1 pt. fixed: I 1 (dω 1 /dt) - ω 2 ω 3 (I 2 -I.
December 9, 2014Computer Vision Lecture 23: Motion Analysis 1 Now we will talk about… Motion Analysis.
4 th SERENA-HEWG Meeting Key Largo, Florida,13-17 May, 2013 page 1 Success of the hybrid modelling technique in simulating the response of the Martian.
Response of the Magnetosphere and Ionosphere to Solar Wind Dynamic Pressure Pulse KYUNG SUN PARK 1, TATSUKI OGINO 2, and DAE-YOUNG LEE 3 1 School of Space.
Particle A particle is an object having a non zero mass and the shape of a point (zero size and no internal structure). In various situations we approximate.
Module 6Aberration and Doppler Shift of Light1 Module 6 Aberration and Doppler Shift of Light The term aberration used here means deviation. If a light.
Figure 1 E conv V SW B IMF E conv X[R M ] X[R M ] E conv V SW B IMF E conv a) c) b) d)
Particle on a Ring An introduction to Angular Momentum Quantum Physics II Recommended Reading: Harris, Chapter 6.
Advanced EM -Master in Physics ACCELERATION FIELDS: THE RADIATION Back to the (Schwartz) formula for the acceleration fields: Fairly complicated,
Observation of high kinetic energy density jets in the Earth’s magnetosheath E. Amata 1, S. P. Savin 2, R. Treuman 3, G. Consolini 1, D. Ambrosino, M.F.
AS 3004 Stellar Dynamics Energy of Orbit Energy of orbit is E = T+W; (KE + PE) –where V is the speed in the relative orbit Hence the total Energy is is.
Simultaneous in-situ observations of the feature of a typical FTE by Cluster and TC1 Zhang Qinghe Liu Ruiyuan Polar Research Institute of China
Analysis of Suprathermal Events Observed by STEREO/PLASTIC with a Focus on Upstream Events STEREO SWG - 20 Meredith, NH October 27-29, 2009 Josh Barry,
Lecture III Curvilinear Motion.
MULTI-INSTRUMENT STUDY OF THE ENERGY STEP STRUCTURES OF O + AND H + IONS IN THE CUSP AND POLAR CAP REGIONS Yulia V. Bogdanova, Berndt Klecker and CIS TEAM.
Multiple Ion Acceleration at Martian Bow Shock M. Yamauchi 1, Y. Futaana 1, A. Fedorov 2, R.A. Frahm 3, E. Dubinin 4, R. Lundin 1, J.-A. Sauvaud 2, J.D.
Derivative Examples 2 Example 3
SEPT/STEREO Observations of Upstream Particle Events: Almost Monoenergetic Ion Beams A. Klassen, R. Gomez-Herrero, R. Mueller-Mellin and SEPT Team, G.
OPTICAL INSTRUMENTS PRESENTED BY: 1. ANA ALINA 2. FIRDIANA SANJAYA.
Foreshock and planetary size: A Venus-Mars comparison M. Yamauchi, Y. Futaana, R. Lundin, S. Barabash, M. Holmstrom (IRF, Kiruna, Sweden) A. Fedorov, J.-A.
Chapter 7 Rotational Motion and The Law of Gravity.
Ch 9.6: Liapunov’s Second Method In Section 9.3 we showed how the stability of a critical point of an almost linear system can usually be determined from.
R. Maggiolo 1, M. Echim 1,2, D. Fontaine 3, A. Teste 4, C. Jacquey 5 1 Belgian Institute for Space Aeronomy (IASB-BIRA); 2 Institute.
Data-Model Comparisons
Mass-loading effect in the exterior cusp and plasma mantle
Boyce/DiPrima 9th ed, Ch 9.6: Liapunov’s Second Method Elementary Differential Equations and Boundary Value Problems, 9th edition, by William E. Boyce.
Stochastic Acceleration in Turbulence:
M. Yamauchi1, I. Dandouras2, H. Reme2,
Ion Pickup Phenomenon upstream of Mars observed by ASPERA 3
Force on an Electric Charge Moving in a Magnetic Field
Mars, Venus, The Moon, and Jovian/Saturnian satellites
Force on an Electric Charge Moving in a Magnetic Field
Force on an Electric Charge Moving in a Magnetic Field
M. Yamauchi1, Y. Futaana1, R. Lundin1, S. Barabash1, M. Wieser1, A
MDI Global Field & Solar Wind
Multiple Ion Acceleration at Martian Bow Shock
Multiple Ion Acceleration at Martian Bow Shock
solar wind – bow shock - magnetosheath
Magnetic Fields Exert Forces on Moving Charges
Mars, Venus, The Moon, and Jovian/Saturnian satellites
Presentation transcript:

IMF derivation from Pickup Ions observed by ASPERA UT UT UT M. Yamauchi B ion ion motion in velocity space is a ring! (spiral motion in real space)

In-coming directions of ions Azimuth scan  Elevation scan  Electric scan IMA

Ion motion with V 0 =0 Viewing from +B Viewing from +E Initial  velocity to B is V 0 cos  velocity space trajectory V* X VYVY VXVX V* Y V* Z VZVZ V (SW frame) = V* (Martian frame) + V SW B 3-D view Ring  2D  minimum variance direction (N) is parallel to B! V 0 =0 in Martian frame means V 0 = -V SW in SW rest frame where E=0.  simple spiral motion,  ring trajectory in velocity space.

, ELS (ch8) + IMA  = 5~15  = 4  = 3  = 2  = 1 SW ring MEX orbit (light blue) during UT in the cylindrical MSO coordinates. R 2 = Y 2 +Z 2. average IMB average BS Mars

Distribution in velocity space MSO (XYZ) MVM (LMN)

Manual method vs. Automatic method Manual Automatic

However, IMA orientation is not always ideal UT All ch8

Aligned in the azi-direction (points 2, 3, 4, 5)  Linear alignment (small data range in M direction) IMA IMA light ion (H+ and He++), 3~8 keV  =5~14  =15  =1  =2  =3  =4 Viewing from +B Viewing from +E

general V 0 ≠0 case  MAX Minimum variance method gives clear L direction (// ±E), but not M & N directions.  We may not use ±N as estimate of B direction, but (1) E x V SW gives B Y /B Z orientation ! (2) B X /B (or  ) can be obtained intuitively

Check item (1) Alignment direction of the ring data by IMA ≈ Maximum variance direction (L X, L Y, L Z ) where L X << 1  B T =(0, B Y, B Z ) // V SW x E // (0, L Z, -L Y ) (2) Sign of B : If L = evolution direction, then sign(B Z ) = - sign(L Y ) (3) Tilt toward X (=  ) *  ' = angle between max energy (  MAX ) direction and SW direction * Ratio k = V MAX /V SW = (  MAX /  SW ) 1/2 If V 0 = 0, two angles must be the same, i.e.,  ' = , and k = cos(  )  If cos(  ') = k, most likely  =  '

Result Using (3)~(6)  Changing IMF for event 0608 UT, northward IMF, X tilt ~ +35~40°, Y tilt ~ -10° 0613 UT, northward IMF, X tilt ~ +35°, Y tilt ~ -45° 0623 UT, northward IMF, X tilt ~ +20°, Y tilt ~ -30° 0633 UT, X tilt > +40° Using (1)~(2)  Constant IMF for event UT, dawn-dusk oriented IMF, X tilt ~ 20°

Procedure (1) Manually select the ring distribution. (2) Apply the minimum variance method to determine L, M, and N. If the ring data is well arranged into a partial circle, ±N // B If not, (3) Examine |L X | < 0.3. If yes, L // -E SW. If not, remove the direction that corresponds to the lowest energy from the selected set of data and re-calculate a new L. (4) Manually obtain  MAX and  '. (5) Check if  MAX /4  SW ≈ cos 2 (  ') is satisfied. If yes, we have  ≈  ', where B X /|B| = sin(  ). (6) If possible, identify the evolution direction and determine the sign of L and E SW. B T is parallel to V SW x E SW.

Summary Approximate IMF orientation can be derived from ring-like distributed protons as measured by the IMA. The actual derivation of the ring plane is complicated (see procedure) due to the very limited viewing directions and angular resolution of the instrument.

New work (1) Beam ? event

New work (2) Use magnetosheath event (again) Can we obtain "sign" of B direction?

H+ only (no He++) !  = 3  = 2  = 4  = 3  = 2 SW He ++ Ring H + SW H +

Motion of ring ions Ion motion with V 0 =0 velocity space trajectory V* X VYVY VXVX V* Y V* Z VZVZ V (SW frame) = V* (Martian frame) + V SW B 3-D view

(easy case)

Beam-origin (V 0 ≠ 0) ring distribution

Selected ring data : ~ 1344~1347 UT *1) L = (0.05, -0.02, 1.00) in MSO *2) M = (0.94, -0.34, -0.06) in MSO *3) N = (0.34, 0.94, ) in MSO

Aligned in azimuthal direction  Almost 1-D alignment  Difficult to determine ring "plane"

From ring data at ~0623 UT ( ) V L (km/s) V N (km/s) V M (km/s)

Selected ring data : ~ 0608 UT *1) L = (0.06, 0.99, 0.14) in MSO *2) M = (0.79, 0.04, -0.61) in MSO *3) N = (0.61, -0.15, 0.78) in MSO

Beam-origin Alignment direction of the ring data by IMA ≈ Maximum variance direction (L X, L Y, L Z ) where L X << 1  B T =(0, B Y, B Z ) // V SW x E // (0, L Z, -L Y ) Sign of B If L = evolution direction, sign(B Z ) = - sign(L Y ) Tilt toward X (=  ) *  ' = angle between max energy (  MAX ) direction and solar wind direction * Ratio k = V MAX /V SW = (  MAX /  SW ) 1/2 If V 0 = 0, two angles must be the same, i.e.,  ' = , and k = cos(  )  If cos(  ') = k, most likely  =  '  MAX