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1
Intelligence, Surveillance, and Reconnaissance (ISR) Programs: Issues for Congress
In: DTIC (2005)
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2
Intelligence, Surveillance, and Reconnaissance (ISR) Programs: Issues for Congress
In: DTIC (2004)
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3
Israel's Quest for Satellite Intelligence
In: DTIC (2001)
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4
The U.S. and South Asia: Partners of Convenience; Global Neighbors of Necessity
In: DTIC (1998)
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5
CORONA and the Intelligence Community
In: DTIC (1996)
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6
Oceanographic Expert System: Potential for TESS(3) Applications
In: DTIC AND NTIS (1992)
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7
Eye Spy: The Utility of Strategic Satellite Reconnaissance
In: DTIC AND NTIS (1990)
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8
Worldwide Report, Telecommunications Policy, Research and Development, No. 268.
In: DTIC AND NTIS (1983)
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9
ON THE ACCURACY OF THE ORBITAL ELEMENTS OF ARTIFICIAL EARTH SATELLITES (O Tochnosti Elementov Orbit Iskusstvennykh Sputnikov Zemli)
In: DTIC AND NTIS (1969)
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10
MOTION OF THE EARTH'S POLES AND ASTRO-GEODETIC WORKS (Dvizhenie Polyusov Zemli i Astronomogeodezicheskie Raboty)
In: DTIC AND NTIS (1969)
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11
COMBINED METHOD OF ADJUSTING A SPACE TRIANGULATION (KOMBINIROVANNII METOD URAVNIVANIYA KOSMICHESKOI TRIANGULYATSII)
In: DTIC AND NTIS (1968)
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12
A MAGNETIC MAP OF THE BRAZILIAN ANOMALY.
In: DTIC AND NTIS (1967)
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13
THE EFFECT OF TANGENTIAL ACCELERATION ON THE MOTION OF A SATELLITE.
In: DTIC AND NTIS (1967)
Abstract: The problem of the motion of a satellite under the effect of tangential acceleration, created by a low-thrust engine, has been solved in other works. This problem is of interest because numerical computations show that the tangential control of the engine thrust approximates well the solution of the problem of the optiminal boost of the satellite. An asymptotic computation of the effect of a reduced tangential acceleration on the motion of a satellite is given in this work by the averaging method. The first approximation solution computed is correct for arbitrary values smaller than a unit of the eccentricity of the satellite unit. The other approximation solution computed is for the problem in the case of near-circular orbits. (Author) ; Vliyanie Kasatelnogo Uskoreniya na Dvizhenie Sputnika, trans. of Prikladnaya Matematika i Mekhanika (USSR), n3 p594-8 1966.
Keyword: *ARTIFICIAL SATELLITES; ACCELERATION; APPROXIMATION(MATHEMATICS); CIRCULAR ORBITS; MATHEMATICAL ANALYSIS; ORBITS; OSCILLATION; Spacecraft Trajectories and Reentry
URL: http://www.dtic.mil/docs/citations/AD0656989
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0656989
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14
AN EXPERIMENT WITH THE CONSTRUCTION OF A GEOMAGNETIC MAP FROM DATA OF AN ARTIFICIAL EARTH SATELLITE.
In: DTIC AND NTIS (1967)
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15
EQUATIONS OF THE MOTION OF AN EARTH'S SATELLITE, TAKING INTO ACCOUNT ATMOSPHERIC RESISTANCE.
In: DTIC AND NTIS (1966)
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16
CONCERNING THE THEORY ON THE DETERMINATION OF THE EARTH'S FIGURE AND DIMENSIONS BY SATELLITE OBSERVATIONS
In: DTIC AND NTIS (1965)
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17
TURN OF THE ORBIT'S PLANE OF ARTIFICIAL EARTH SATELLITE
In: DTIC AND NTIS (1965)
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18
RADIO COMMUNICATIONS WITH ARTIFICIAL SATELLITES OF THE EARTH
In: DTIC AND NTIS (1965)
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19
PROBLEMS IN THE MOTION OF ARTIFICIAL CELESTIAL BODIES.
In: DTIC AND NTIS (1964)
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20
PROBLEMS IN THE MOTION OF ARTIFICIAL CELESTIAL BODIES.
In: DTIC AND NTIS (1964)
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