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To the interpretation of the osculations of orbits and the in-space launching point of artificial cosmic bodies

Karel Mišoň — 1969

Aplikace matematiky

The case of transferring the rocket from the prescribed path of departure to the transfer orbit osculating another given complanar rocket trajectory of arrival is studied. The introducing to the transfer orbit is realized only by a change of the modulus of velocity of the rocket without changing the flight direction. The requirement of osculating the two conic sections leads to a solution of an algebraic-trigonometric system which is numerically labourious. The prescription of the position of the...

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