1987
DOI: 10.1109/proc.1987.13706
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Crosslink architectures for a multiple satellite system

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Cited by 41 publications
(11 citation statements)
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“…Similarly, in [14], nodes in a spread spectrum system generate pseudo random schedules in order to reduce medium access interference. Apart from [15], which is targeted at satellite systems, existing schemes have mainly considered the use of pseudo-random time-slots in an effort to reduce collisions. For example, the MAC presented by Cao et al [9] requires nodes to assign a unique seed to each of their neighbors.…”
Section: Related Workmentioning
confidence: 99%
“…Similarly, in [14], nodes in a spread spectrum system generate pseudo random schedules in order to reduce medium access interference. Apart from [15], which is targeted at satellite systems, existing schemes have mainly considered the use of pseudo-random time-slots in an effort to reduce collisions. For example, the MAC presented by Cao et al [9] requires nodes to assign a unique seed to each of their neighbors.…”
Section: Related Workmentioning
confidence: 99%
“…For example, the average propagation delay at time 300 is .029 seconds for N3 and .034 seconds for N10, causing different queue sizes even though the traffic rates are the same. AI IocLc tc-hed1r-n .5 pk ts/sec ) 1 viding congestion "snapshots." The total simulated time shown corresponds to one-half of a full orbit.…”
Section: Examplesmentioning
confidence: 99%
“…A wide variety of such networks can be configured depending upon the particular mission requirements. They may range from networks with tightly stabilized and precision controlled satellites to networks that may employ a very large number of simply stabilized low-cost satellites whose proliferation provides a high degree of survivability [1]. Design of such networks is difficult due to the large number of variables associated with physical topologies, communications protocols, and operational requirements such as build-up, replenishment and reconfigurability.…”
Section: Introductionmentioning
confidence: 99%
“…A single satellite with a 12 h period in an elliptical orbit with an apogee at 40, 0o0 km and inclined at an angle of 63" from the *Now with INMARSAT H.Q. London equator can achieve an 8 h coverage of the visible earth, nearly from the equator to the poles. An example of such an orbit is the Molniya, from the well known Soviet satellite communication ~y s t e m .~ Recent studies have shown interest in 24 h period satellites, referred to as the Tundra t~p e .~,~ For both types, 24 h continuous coverage entails the use of several satellites.…”
Section: Introductionmentioning
confidence: 99%