
SATELLITE AND SPACE COMMUNICATIONS
27-3
Advances in rocketry and microwave engineering
inspired early proposals for communications satellites.
Experiments of the late 1950s and early 1960s culmi-
nated in the successful launch of
Early Bird
in 1965,
by Comsat (the Communications Satellite Corpora-
tion), established by act of the US Congress for this
purpose, from which time satellite communications
can be dated.
In
space systems, earth stations operate in conjunc-
tion with orbiting spacecraft that probe the space
environment-the earth as observable from space, the
moon,
a
planet, or any other celestial body.
In
satellite
communications systems, two or more stations located
on or near the earth communicate via satellites that
serve as relay stations in space.
In
both instances, con-
trol and monitoring of the spacecraft require that
telemetry and command links be added to the main
function of the mission. Space systems include terres-
trial missions (e.g., earth and/or sea surface observa-
tions of different kinds), weather satellites, and
navigation satellites. Beyond the earth, space systems
can be classified in terms of the mission range (i.e.,
cislunar, lunar, translunar, or planetary)
as
well
as
in
terms of the specific nature of the observations to be
canied
out.
Communications satellite systems are classified in
terms of their territorial coverages, e.g., global,
regional, or national (domestic); in terms of the type of
services offered, e.g., fixed, mobile, maritime, aero-
nautical, etc., or point-to-point, broadcasting, commer-
cial, military, amateur, experimental, etc.; or in terms
of their orbit, e.g., geostationary (GEO), medium earth
orbit
(MEO),
or low earth orbit (LEO).
Regulatory bodies (FCC, ITU) often categorize
capabilities by service. In satellite communications,
there are three broad service categories: fixed, mobile,
and broadcast. Fixed satellite services
(FSS)
cover
links between satellites and fixed (nonmoving) earth
stations. Mobile service covers satellite links to sta-
tions that may be in motion (mobile), including ships
(maritime mobile [MMSS]), aircraft (aeronautical
mobile [AMSS]), and land vehicles (land mobile
[LMSS]).
Broadcast services include TV (DBS-TV)
and audio (DBSA). It should be noted that services are
evolving, and while the FCC and ITU designations
will change very slowly, the reality is changing rather
more quickly,
as
will be discussed briefly in the section
on Other Services below. Examples of this are DTH
(direct to home), which covers a broader swath than
just TV as interactive services emerge, and DARS
(digital audio radio service), which covers nationwide
satellite digital radio to automobiles (and possibly
homes).
The ITU internationally and the FCC in the United
States allocate frequency bands for the use of these
services, and where the bands overlap, they designate
which service has priority.
The environment of space affects the design of com-
munications systems in several ways that make it dif-
ferent from the design of terrestrial systems. Major
differences are:
A.
B.
C.
Space and satellite communications systems
can and often do cover distances far exceeding
those encountered on earth.
As
spacecraft power and allocated bandwidth
are limited resources, trade-offs of space and
earth segment design characteristics affect the
overall system cost.
As
the conditions along the signal paths are
much more time invariant in space than on
earth, it is possible to design space-to-space
communications systems with great precision.
Space+arth and earth-space signal paths
traverse the troposphere and ionosphere and are
subject
to
the vagaries thereof, but these tend
not to be
so
severe
as
those encountered on long
terrestrial paths (see section on Propagation).
Three categories characterized by different environ-
mental constraints can be identified, as follows.
Spacecraft-to-Spacecraft:
In principle, the designer
has maximum freedom in the choice of the oper-
ating frequency. The major difficulty resides in
maintaining tracking between spacecraft.
Earth-to-Spacecraft (Up-Link):
The choice of the
operating frequency is primarily determined by
the availability of spectral windows in the signal
path. The window boundaries are dictated by
absorption and dispersion phenomena in the iono-
sphere and troposphere, the attenuation and depo-
larization effects of hydrometeors (rain, snow,
ice, etc.,) and also by the spectral and spatial dis-
tributions of natural noise sources. On earth, the
ubiquitous availability of electrical power and the
relatively benign environment make it possible
to
use large amounts of transmitter power enhanced
by high-gain, large antennas that must be pre-
cisely aimed at the spacecraft.
Spacecraft-to-Earth (Down-Link)
:
Launch-vehicle
limitations restrict the size of the spacecraft trans-
mit and receive antennas, and the spacecraft
receiver is affected by the background noise of
the earth. The spacecraft transmitter is limited by
the power available, which in turn is limited by
the size of the solar cell arrays, again launch-
vehicle limited. These limitations are increasingly
less severe. Spacecraft originally (1963-1965)
had dipole antennas and only
a
few hundred watts
of
dc electrical power from solar arrays.
In
the
year
2000,
spacecraft on orbit had 15-meter
antennas and dc power up to 15 kW.
In earlier days, limited spacecraft transmitter power
and antenna sizes (gain) were compensated for by
electrically large earth-station receive antennas and
low-noise receivers. Today, spacecraft eirps (equiva-
lent isotropically radiated power) have reached the