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Next Generation of Magnetosphere-Ionosphere-Thermosphere Coupling Models

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Next Generation of Magnetosphere-Ionosphere-Thermosphere Coupling Models P. Song University of Massachusetts Lowell Acknowledgments: V. M. Vasyli nas, and J. Tu – PowerPoint PPT presentation

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Title: Next Generation of Magnetosphere-Ionosphere-Thermosphere Coupling Models


1
Next Generation of Magnetosphere-Ionosphere-Thermo
sphere Coupling Models
  • P. Song
  • University of Massachusetts Lowell
  • Acknowledgments V. M. Vasyliunas, and J. Tu
  • Conventional Models Steady-state coupling
    between magnetosphere and ionosphere
  • (Steady state) Ohms law with constant
    conductivities
  • Electrostatic potential
  • Constant magnetic field self-consistency breaks
    when there are currents and spatially varying
    electric field
  • Dynamics in the magnetosphere does not couple
    dynamically to the ionosphere
  • Ionospheric horizontal motion is not derived
    with dynamic effects
  • Observationally, difficult to explain the
    overshoot of an onset (lt 30 min)
  • New generation models
  • Inductive B changes with time
  • Dynamic in particular ionospheric motion
    perpendicular to B
  • Multi fluid allowing upflows and outflows of
    different species
  • Wave propagation/reflection overshoots
  • Summary

2
M-I Coupling
  • Explain the observed ionospheric responses to
    solar wind condition/changes, substorms and
    auroras etc. and feedback to the magnetosphere
    (not to simply couple codes)
  • Conventional Ohms law in the neutral framegt
    the key to coupling
  • Derived from steady state equations (no
    ionospheric acceleration)
  • Conductivities are time constant
  • J and E are one-to-one related no dynamics
  • Magnetospheric Approach
  • Height-integrated ionosphere
  • Neutral wind velocity is not a function of height
    and time
  • Ionospheric Approach
  • Structured ionosphere
  • Magnetosphere is a prescribed boundary
  • Not self-consistent steady state equations to
    describe time dependent processes (In steady
    state, imposed E-field penetrates into all
    heights)
  • Do not solve Maxwell equations

3
Field-aligned Current Coupling Models
Full dynamics
Electrostatic
Steady state (density and neutrals time varying)
  • coupled via field-aligned current, closed with
    Pedersen current
  • Ohms law gives the electric field and Hall
    current
  • electric drift gives the ion motion

4
M-I Coupling (Conventional)
  • Ohms law in the neutral frame the key to
    coupling
  • Magnetospheric Approach
  • Height-integrated ionosphere
  • Current conservation
  • Neutral wind velocity is not a function of height
    and time
  • No self-consistent field-aligned flow
  • No ionospheric acceleration
  • Ionospheric Approach
  • Structured ionosphere
  • Magnetosphere is a prescribed boundary
  • Not self-consistent steady state equations to
    describe time dependent processes (In steady
    state, imposed E-field penetrates into all
    heights)
  • Do not solve Maxwell equations

5
M-I coupling model Driven by imposed E-field in
the polar cap
6
Conventional Model Results Penetration E-field
7
M-I Coupling (Conventional)
  • Ohms law in the neutral frame the key to
    coupling
  • Magnetospheric Approach
  • Height-integrated ionosphere
  • Neutral wind velocity is not a function of height
    and time
  • Ionospheric Approach
  • Structured ionosphere
  • Magnetosphere is a prescribed boundary
  • When upper boundary varies with time, the
    ionosphere varies with time (misinterpreted as
    dynamic coupling)
  • Not self-consistent steady state equations to
    describe time dependent processes (In steady
    state, imposed E-field penetrates into all
    heights)
  • Do not solve Maxwells equations
  • No wave reflection
  • No fast and slow modes in ionosphere (force
    imbalance cannot propagate horizontally)
  • No ionospheric acceleration

8
Theoretical Basis for Conventional Coupling Models
  • B0 gtgtdB and B0 is treated as time independent
    in the approach, and dB is produced to compare
    with observations
  • not a bad
    approximation

  • questionable for short time scales dynamics

  • questionable for short time scales
  • Time scale to reach quasi-steady state
    dtdLdB/dE
  • given dL, from the magnetopause to ionosphere,
    20 Re
  • dB, in the ionosphere, 1000 nT
  • dE, in the ionosphere, for V1 km/s, 6x10-2 V/m
  • dt 2000 sec, 30 min, substorm time scale!
  • Conventional theory is not applicable to
    substorms, auroral brightening!

9
Ionospheric Dynamic Processes
Epoch analysis showing on average an overshoot in
ionospheric velocity for 30 min.
An overshoot lasting 40 min was seen on ground
but not in geosynchronous orbits indicating the
overshoot is related to the ionospheric processes
Huang et al, 2009
10
North Pole, Winter Solstice
11
Ion-neutral Interaction
  • Magnetic field is frozen-in with electrons
  • Plasma (red dots) is driven with the magnetic
    field (solid line) perturbation from above
  • Neutrals do not directly feel the perturbation
    while plasma moves
  • Ion-neutral collisions accelerate neutrals (open
    circles), strong friction/heating
  • Longer than the neutral-ion collision time, the
    plasma and neutrals move nearly together with a
    small slippage. Weak friction/heating
  • On very long time scales, the plasma and neutrals
    move together no collision/no heating

12
Ionosphere Reaction to Magnetospheric Motion
  • Slow down wave propagation (neutral inertia
    loading)
  • Partial reflection
  • Drive ionosphere convection
  • Large distance at the magnetopause corresponds to
    small distance in the ionosphere
  • In the ionosphere, horizontal perturbations
    propagate in fast mode speed
  • Ionospheric convection
  • modifies magnetospheric
  • convection
  • (true 2-way coupling)

13
Global Consequence of A Poleward Motion
  • Antisunward motion of open field line in the
    open-closed boundary creates
  • a high pressure region in the open field region
    (compressional wave), and
  • a low pressure region in the closed field region
    (rarefaction wave)
  • Continuity requirement produces convection cells
    through fast mode waves in the ionosphere and
    motion in closed field regions.
  • Poleward motion of the feet of the flux tube
    propagates to equator and produces upward motion
    in the equator.
  • Ionospheric convection will drive/modify
    magnetospheric convection

14
Expected Heating Distribution
sun
  • For uniform conductivity, velocity pattern
    coincides with the magnetic perturbation.
  • FAC forms at the center of the convection cells
  • Poynting flux is proportional to V2, weakest at
    the center of convection cells
  • Neglecting the heating from precipitation
    particles,
  • Conventional model (EJ paradigm) predicts
    heating, J2/?p, is highest at the FAC
  • New model (BV paradigm) predicts heating,
    ?in?iV2, is highest at compression region of
    dayside and nightside cusps and strong along the
    noon-midnight meridian

15
Consequence of Heating
  • Energy equation
  • Neglecting radiative loss, R, and heat conduction
  • Enhanced temperature and upward motion are
    expected

16
Basic Equations
  • Continuity equations
  • Momentum equations
  • Temperature equations
  • Faradays Law and Ampere's Law

s e, i or n, and es -e, e or 0
Field-aligned flow allowed
17
Simplifying Assumptions (dt gt 1sec)
  • Charge quasi-neutrality
  • Replace electron continuity with
  • Neglecting the electron inertial term in the
    electron momentum equation
  • Electric field, E, can be eliminated in other
    equations
  • electron velocity will be calculated from current
    definitions.

18
Momentum equations without electric field E
19
Numeric Consideration
Large collision frequencies make equations
strongly stiff
is very large at low altitude, e.g., at 80 km
s-1
Extremely small time step (lt 10-6 s) is required
for explicit algorithms to be numerically stable.
Implicit algorithms are necessary
20
1-D Stratified Ionosphere/thermosphere
  • Equation set is solved in 1-D (vertical), assume
    ?BltltB0.
  • Neutral wind velocity is a function of height
    and time
  • The system is driven by a change in the motion
    at the top boundary
  • No local field-aligned current horizontal
    currents are derived
  • No imposed E-field E-field is derived.
  • test 1 solve momentum equations and Maxwells
    equations using explicit method
  • test 2 use implicit method (increasing time
    step by 105 times)
  • test 3 include continuity and energy equations
    with
  • field-aligned flow

2000 km
500 km
21
Dynamics in 2-Alfvén Travel Time
x antisunward y dawnward, z upward, B0
downward On-set time 1 sec Several runs were
made the processes are characterized in Alfvén
time Building up of the Pedersen current
Song et al., 2009
22
30 Alfvén Travel Time
  • The quasi-steady state is reached in 20 Alfvén
    time.
  • During the transition, antisunward flow in the
    F-layer can be large
  • During the transition, E-layer and F-layer have
    opposite dawn-dusk flows
  • There is a current enhancement for 10 A-time,
    more in Pedersen current

Song et al., 2009
23
Neutral wind velocity
  • The neutral wind driven by M-I coupling is
    strongest in F-layer
  • Antisunward wind continues to increase

Song et al., 2009
24
After 1 hour, a flow reversal at top boundary
  • Antisunward flow reverses and enhances before
    settled
  • Dawn-dusk velocity enhances before reversing
    (flow rotates)
  • The reversal transition takes slightly longer
    than initial transition
  • Larger field fluctuations

Song et al., 2009
25
After 1 hour, a flow reversal at top boundary
Pedersen current more than doubled just after
the reversal
Song et al., 2009
26
Electric field variationsNot Constant!
Electric field in the neutral wind frame E E
unxB Not Constant!
Song et al., 2009
27
Heating rate q as function of Alfvén travel time
and height. The heating rate at each height
becomes a constant after about 30 Alfvén travel
times. The Alfvén time is the time normalized by
tA, which is defined as If the driver is at
the magnetopause, the Alfvén time is about 1
min. Height variations of frictional heating
rate and true Joule heating rate at a selected
time. The Joule heating rate is negligibly small.
The heating is essentially frictional in nature.
Tu et al., 2011
28
Heating rate divided by total mass density
(neutral mass density plus plasma mass density)
as function of Alfvén travel time and height. The
heating rate per unit mass is peaked in the F
layer of the ionosphere, around about 300 km in
this case.
Time variation of height integrated heating rate.
After about 30 Alfvén travel times, the heating
rate reaches a constant. This steady-state
heating rate is equivalent to the steady-state
heating rate calculated using conventional Joule
heating rate J(EunxB) defined in the frame
moving with the neutral wind. In the transition
period, the heating rate can be two times larger
than the steady-state heating rate.
Tu et al., 2011
29
Summary
  • A new scheme of solar wind-magnetosphere-ionosphe
    re-thermosphere coupling is proposed
  • Including continuity, momentum equation, and
    energy equation for each species of multi fluids
  • Including Maxwells equations
  • Including photochemistry
  • No imposed E-field is necessary, and no imposed
    field-aligned current is necessary
  • 1-D studies steady state, wave dispersion
    relation and attenuation, time dependence,
    ionospheric heating, coronal heating
  • An implicit numerical scheme has been developed
    to make the time step large (5 orders) enough for
    global simulations
  • In 1-D simulations, there are 4 major differences
    between the dynamic (and inductive) coupling and
    the steady-state coupling
  • Transient time for M-I equilibrium not Alfvén
    travel time, but 10-20 ? tA 20-30 min.
  • Reflection effect enhanced Poynting flux and
    heating rate during the dynamic transient period
    can be a factor of 1.5 greater than that given in
    of steady-state coupling
  • Plasma inertia effect velocity, magnetic field,
    and electric field perturbations depend on
    density profile during the transition period
  • Field-aligned upflow allowed
  • In 2-D and 3-D ionosphere can be an active
    player in determining magnetospheric convection.
    It can be the driver in some regions.
  • Using Ohms law in the neutral wind frame in
    conventional M-I coupling will miss
  • the dynamics during the transition lt 30 min
  • neutral wind acceleration gt 1 hr.

30
Comparison of Steady-state Coupling with Dynamic
Coupling
  • Coupling speed Vphase
  • Steady-state Coupling
  • Original model (Vasyliunas, 1970, Wolf, 1970)
    not specific, presumed to be VA
  • Implemented in simulations ? (instantaneously)
  • Dynamic Coupling Vphase a1/2 VA (? is
    neutral inertia loading factor)
  • Coupling time dt
  • Steady-state Coupling
  • Original model not specified,
  • Implemented in simulations 0
  • Dynamic Coupling

12 min (Alfvén transient) 30 min (M-I
equilibrium) 13 hours (neutral acceleration)
31
Comparison of Steady-state Coupling with Dynamic
Coupling, cont.
  • Reflection
  • Steady-state Coupling
  • Original model Multiple reflections assumed,
    V,B
    final result, (depends on ionospheric
    conductivity)
  • Implemented in simulations No reflection,
  • EEinc, V and dB are derived
  • Dynamic Coupling TotalIR for both dB and V
  • Reflection coefficient ? depends on gradient
    (height) and frequency (time lapse)
  • Reflection may be produced continuously over
    height
  • Incident perturbation may consist of a spectrum
    dispersion effect
  • A phase delay f due to propagation to and from
    the reflection point

32
Comparison of Steady-state Coupling with Dynamic
Coupling, cont.
  • Velocity perturbation V
  • Steady-state Coupling
  • Original model Include final result of multiple
    reflections
  • Implemented in simulations
  • Dynamic Coupling For single A-wave, parallel
    propagation, weakly damped (there are reflected
    waves)

33
Comparison of Steady-state Coupling with Dynamic
Coupling, cont.
  • Magnetic perturbation dB
  • Steady-state Coupling not included as part of
    model evolution,
  • calculated from J
  • Dynamic Coupling For single A-wave parallel
    propagation weakly damped (there are reflected
    waves)
  • Local along B, from
  • B0, V0, dB0, ?i0,
  • Electric field perturbation E
  • Steady-state Coupling
  • Dynamic Coupling For single A-wave parallel
    propagation weakly damped (there are reflected
    waves)
  • Dynamic with reflection

34
Comparison of Steady-state Coupling and Dynamic
Coupling, cont.
  • Current J
  • Steady-state Coupling
  • Dynamic Coupling (derived from dB, current
    continuity satisfied)
  • Poynting vector S
  • Steady-state Coupling Not considered
    explicitly,
  • DC part included implicitly in dissipation
  • Dynamic Coupling For single A-wave parallel
    propagation weakly damped
  • Dynamic with reflection

35
Comparison of Steady-state Coupling with Dynamic
Coupling, cont.
  • Heating Rate q
  • Steady-state Coupling
  • Dynamic Coupling For single A-wave parallel
    propagation weakly damped
  • The perturbations include incident and
    reflected waves
  •  

36
Center for Atmospheric Research of UMass Lowell
(http//ulcar.uml.edu)
  • Staff 23, (4 faculty, 4 students, 3 posdocs, 4
    scientists, 8 regular,)
  • A new group is joining
  • Products
  • Scientific publications (1 book, and 31 papers in
    2011)
  • Ground-based ionospheric sounders ( 5
    systems/yr, list price 0.2 M each)
  • Data/network services ( 80 stations worldwide)
  • Space-borne instrumentation (1 completed
    operation, 1 under development)
  • Rockets, balloons instrumentation (new to the
    center)
  • Collaborators AFRL, NASA Goddard, Max Plank
    Institute, NASA Marshal, Stanford,
  • Funding Air Force, NASA, NSF, International
    science institutions
  • Annual revenues 3 M
  • Office space 12000 sqft
  • Major projects
  • AF Radiation belt remediation 2.5 mil
  • NASA Space Physics 1 mil
  • NSF Space Weather 0.6 mil

37
Space Sciences at the Center for Atmospheric
Research
  • Radio Science
  • Radio wave transmission in plasma
  • Radio wave propagation in plasma
  • Ground penetration radar
  • Space Weather
  • Radiation belt remediation
  • Space weather models
  • plasmasphere,
  • magnetopause,
  • magnetosheath
  • Magnetospheric Physics
  • Magnetosphere-ionosphere coupling
  • Plasmasphere depletion and refilling
  • Energetic particles measurements and analyses
  • ULF wave acceleration of particles
  • Ionospheric Physics
  • Ionospheric Reference model
  • Ionospheric out flow and acceleration
  • Ionospheric disturbance

38
Advanced Technology at the Center for Atmospheric
Research
  • RF Technologies
  • Analog front-end design (receivers/transmitters),
    Low/high power amplifiers, filters, Antenna
    design
  • Digital Up/down-converters, Synthesizers, Pulse
    code modulation, Spectral analysis using FPGAs
    and DSPs, FFTs, filters, FPGA (Altera Stratix
    and Actel Radiation hardened)
  • Mixed AtoD, DtoA
  • General Circuit Board design and layout, Power
    Supply development, Radiation hardened circuit
    technology
  • Computer Hardware Technologies
  • Computer Systems Embedded Computers (SPARC and
    Intel), Embedded microcontrollers (PIC)
  • Enclosures and Backplanes VME chassis,
    CompactPCI chassis, Ruggedized and space flight
    chassis
  • Computer Software Technologies
  • Operating Systems Windows XP, Linux, Embedded
    Real time OS (RTEMS and VxWorks)
  • Languages C, Java, Assembler (Intel X86, PIC
    embedded and DSP)
  • Development Tools
  • ModelSim Verilog
  • Altera development suite (Quartus II)
  • Gnu software development tools

39
Modern Ionosonde and Transmit Antennameasuring
height of the ionosphere and temporal variations
Digisonde DPS
Transmit antenna
40
(No Transcript)
41
Radio Plasma Imager (RPI) on NASA IMAGE
satellite in operation
Launched 25 Mar 2000
42
LORERS Mission
LORERS transmits radio waves to deplete the
radiation particles in radiation belt to protect
LEO satellites
AFRL/DARPA Radiation-Belt-Remediation (RBR)
high-power transmitter under development at the
Center
43
Jupiter Icy Moons Orbiter (2012)
  • To explore the three icy moons of Jupiter and
    investigate their makeup, their history and their
    potential for sustaining life.
  • To develop a nuclear reactor and show that it can
    be processed safely and operated reliably in deep
    space for long-duration deep space exploration.

Planetary Advanced Radio Sounder (PARS) for JIMO
mission under development at the Center
44
Comparison of the Jupiter moons(Icy surface of
Europa)
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