The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration

Details The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration

May 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..339p&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, May-June 1989, p. 339-346. In Russian.

Astronomy and Astrophysics

Astronomy

Celestial Mechanics, Hill Method, Orbit Calculation, Satellite Orbits, Astrodynamics, Differential Equations, Evolution (Development), Polar Orbits, Riccati Equation, Three Dimensional Motion

Scientific paper

The motion of a spacecraft with small transverse acceleration in the
Hill problem is studied. The averaged equations of the three-dimensional
motion are applied to a set of third-order differential equations. This
set permits partial solutions corresponding to two-dimensional motion
and to motion in circular and polar orbits.

Affiliated with

Also associated with

No associations

Rating

The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and The evolution of orbits in the twice-averaged Hill problem under the influence of small transverse acceleration will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1874750