Determination of the intervals and dates of critical illumination conditions for spacecraft instruments

Details Determination of the intervals and dates of critical illumination conditions for spacecraft instruments Determination of the intervals and dates of critical illumination conditions for spacecraft instruments

Jan 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..141i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, Jan.-Feb. 1987, p. 141-147. In Russian.

Physics

Critical Point, Illuminance, Satellite Orbits, Spacecraft Instruments, Sunlight, Temporal Distribution, Circular Orbits, Elliptical Orbits, Geocentric Coordinates, Trigonometric Functions, Vector Analysis

Scientific paper

The paper examines problems involving the determination of the time intervals and dates of critical solar-illumination conditions for the operation of spacecraft instruments. The solution to these problems is based on methods employing the transformation of vector conditions of critical illumination to trigonometric inequalities. Cases of elliptical, circular, and stationary satellite orbits are considered.

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