Journal
Scientific and technical journal «Priborostroenie»
UDK629.7.05
Issue:9 (52)
Download PDF452 Kbyte
The problem of optimization of navigational measurements program on board of a space vehicle is considered. A method is proposed to solve the problem on the basis of the known Rozenbrok computing scheme. The method includes a procedure of random search for detailed analysis of a neighborhood of a point of supposed extremum. Computed results are presented for various values of a space vehicle orbit eccentricity and navigational parameters: two angles “a star — horizon of the Earth” and angular diameter of the Earth.