Report on the Activity
of Commission G
(11 March 2005)
1. Development of Ionospheric observation facility
Multi-functional
Transport Satellite (MTSAT) was successfully launched on 26 February 2005. One of the missions
of the satellite is Satellite-Based Augmentation System (SBAS) supporting GPS
application in aircraft navigation. In order to investigate and evaluate the
ionospheric effects on the GPS signals, Electronic
Navigation Research Institute (ENRI) installed 12 GPS receivers in Ishigaki Island, South of Japan. Five receivers
among them are capable of observing ionospheric
scintillations, and the others are total electron content (TEC). These receivers
are aligned the East-West and North-South baselines with a separation of 100 to
1000 m. Characteristics of plasma bubbles including onset times, density
depletions, drift velocities, significance of scintillations will be observed.
Based on the observations, empirical model of ionospheric degradation of the GPS signals will be
constructed and provided for aviation users and system designers.
STELAB,
Nagoya
University installed an
all-sky airglow imager at the Resolute Bay Observatory (74.7N, 265.1E) in
collaboration with the SRI International. The imager started automatic
measurements from 11 January
2005. Quick-look data (deviation from one-hour running averages to
see gravity waves) are available at
http://stdb2.stelab.nagoya-u.ac.jp/omti/index.html (please see Imager #6.) The
information of filters, exposures, and time resolutions is as
follows.
Resolute Bay
: (74.7N, 265.1E)
All-Sky
Imager #6 (Jan.11, 2005-)
(2x2 binning = 256x256pixels)
OI
(557.7nm, expo: 30s), OI (630.0nm, 30s),
OH-bands(2s),
Na (589.3nm, 30s) : every
2min
OI
(777.4nm, 45s) : every 20 min
2. Observation
Campaigns
The rocket
campaign DELTA (Dynamics and Energetics of the Lower
Thermosphere in Aurora) was carried out on 13 December 2004 in
Norway. The sounding rocket S310-35
was launched at 0:33 (UT) to measure the ionospheric
plasma and neutral gasses during the diffuse aurora. Ground-based observations
were simultaneously made by using EISCAT radar and Fabry-Perot interferometer during the rocket flight. This
campaign aimed to clarify the driving factor of strong neutral wind, in
particular, horizontal wind. The new experiment in this campaign is neutral
(N2) temperature measurement which is planned to measure the neutral
atmospheric heating due to the auroral precipitation
or joule heating. It is possible to discuss the physical process of atmospheric
heating and effect on the driving wind system in comparison with the results of
other instruments as the electron density, temperature or aurora glowing
intensity. Electron number density measurement was made by using instrument
provided by the Tohoku University group, namely, the NEI instrument on-board the
S310-35. NEI is the impedance probe which is developed by Oya [1966]. The NEI sensor was BeCu ribbon antenna, and extended at the altitude of 72.9
km. During the ascending period, electron density enhancements were observed in
the altitude ranges from 100 to 110 km and from 125 to 130 km with the electron
densities of about 1~106 cm-3 and 6~105
cm-3, respectively. In the descending phase, electron density
enhancement was in the altitude range from 108 to 115 km, and there were many
periodic density fluctuations due to the rocket wake. These electron density
enhancements seem to be associated with the enhancement of neutral temperature
at auroral altitudes. It is interesting to compare
with the other observation results during the DELTA campaign, not only the
on-board instruments but also ground-based instruments as the EISCAT
radar.
3. Data
Analyses
For clarifying the structure and occurrence
characteristics of the ionization ledge, the topside sounder data observed by
the Ohzora (EXOS-C) and ISIS-2 satellites in the
equatorial ionosphere were analyzed. We analyzed topside ionograms of 19 and 430 passages observed by Ohzora in March and May, 1987 and ISIS-2 in 1973-1979,
respectively. Also the variations of the geomagnetic field were analyzed to
deduce the electric field. The ionization ledge was found in a dip latitude
range from –13.5 to 19.3, at the limited region around the dip equator. The
ionization ledge appears in the local time sector from 9-11 LT to 0-2 LT. The
occurrence probability is highest in the noon sector and tends to decrease gradually with local
time. These results are consistent with the previous studies of the ionization
ledge. The occurrence probability of the ionization ledge is higher in equinox
seasons and lower in solstice seasons, which is consistent with the seasonal
variation of the upward plasma drift derived by the AE-E satellite. Comparing
with the eastward electric field deduced by the variations of the horizontal
component of the geomagnetic field, the occurrence probability of the ionization
ledge obtained by analyzing the Ohzora sounder data
tends to be higher when the time integrated electric field shows a large value.
These results indicate that the upward drift caused by the E~B
term is the major source of the generation mechanism of the ionization ledge as
reported in the previous studies. On the other hand, the present data analysis
revealed the following important character of the ionization ledge. The ledge
altitude has no clear dependence on the local time. However, the magnitude of
the plasma density enhancement tends to become higher depending on the local
time. The ionization ledge sometimes occurred even when the magnitude of the
time integrated electric field variation was small. Therefore, in addition to
the electric field effect, another control mechanism is possibly affecting the
generation or containment of the ionization ledge structure. Majority of the
character of the ionization ledge is basically the same with the character of
the F3 layer in terms of the local time
dependence of occurrence (Balan et al., 1998).
However, the seasonal dependence of the occurrence probability has a tendency
contrary to that of the F3 layer reported by Balan et al. (2000).
4. Ionospheric response to the December 26, 2004 Sumatra-Andaman
Islands
Earthquake
Total
electron content fluctuations as observed by the meridional GPS receiver chain over Indonesia and
Thailand (Chiang Mai, Bangkok, Chumphon, Medan, and Padang) were analyzed by the
scientists of STEL, Nagoya University. In response to the atmospheric
perturbation over the epicenter, the ionospheric total
electron content increased stepwise by more than 7 TEC units (1TEC
unit=1~1016 electrons/m3). They interpret the TEC
fluctuation was caused by a sonic wave launched by the earthquake, and its
efficiency to modify the ionosphere depended on the geometry of the earthfs
magnetic field inclination and the sonic wave propagation path, which can
explain the observed geographical and temporal changes in the TEC
perturbation.
@@@@@@@@@@@@@@@@@@@TEC perturbation caused by the earthquake
| |
@@
Chiang Mai,
Bangkok, Chumphon (NICT), Medan (SOPAC),
Padang (STEL, Nagoya U.)
ͺ
0058 UT:
Earthquake
The first signal was detected 14 min after the earthquake at Padang
5. Coming
Workshops
(1)
Space
Environment Center Space Weather Week, in Boulder, CO, USA, 5-8 April 2005,
http://www.sec.noaa.gov/sww/
(2) The 11th International Ionospheric Effects Symposium, in Alexandria,
VN, USA, 3-5 May 2005,
http://www.ies2005.com/
(3) The 11th International Symposium on
Equatorial Aeronomy (ISEA-11), in Taipei, Taiwan, 9-14
May 2005, http://140.115.111.70/ISEA-11/3rd_circular.html
(4) IAGA
Scientific Assembly, in
Toulouse, 18-29
July 2005,
http://www.iugg.org/IAGA/index.htm
(5) URSI General Assembly, in New Delhi, India, 23-29 October 2005,
http://www.ursiga2005.org/ecm/index.php
During URSI
General Assembly cited above, a General Lecture and an intercommission session on Solar Power Satellite (SPS) are
arranged as below. Dr. Michael Rietveld of EISCAT will
also give a talk entitled, "Interactions between microwave power transmissions
from a solar power station and the ionosphere-atmosphere system" based on the
recommendation of Commission G.
U1 - GENERAL
LECTURE 1 (Monday 24/10/2005 14:00-15:20)
gSolar Power
Satellite (SPS) for Sustainable Clean Energy Humanosphereh by Prof. Hiroshi
Matsumoto
HX -
INTERCOMMISSION SESSION - Solar power satellites (SPS)
(I,C,P)
(Tuesday
25/10/2005 14:00-16:20)
Session subjects include: passive and active microwave devices, antenna and
rectenna, huge antenna arrays, retrodirective systems, antennas in plasma, self
calibration, compatibility with telecommunications and radio astronomy, radio
frequency interference and electromagnetic compatibility (RFI and EMC), the
interaction of heavy ions ejected from the electric spacecraft propulsion
engine. (Conveners: H.Kozo Hashimoto, Japan: kozo@rish.kyoto-u.ac.jp and D. Tatsuo Itoh, USA:
itoh@ee.ucla.edu)
(Prepared by
T. Maruyama and M. Yamamoto)