Add to ORKGComputer simulation of orbit estimation satellites has been developed. The combined effects of the zonal harmonics of the Earth gravitational field and the sun and moon attraction effects on the orbital elements , the right ascension of ascending nodes and the argument of perigee ,were investigated. Orbit estimation is based on the iterative solution of Kepler's equation by using Newton method
Application of celestial mechanics to artificial satellite orbit calculations using orbit perturbati...
An analysis is carried out which considers the relationship of orbit mechanics to the satellite navi...
Typescript.Thesis (Ph. D.)--University of Hawaii, 1967.Bibliography: leaves [91]-103.ix, 103 l illus...
The effects of atmosphere drag and zonal harmonics J2 of the gravitational potential of the Cosmos14...
The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orb...
The trajectory analysis of a celestial object orbiting another body is the basis for all other, more...
Abstract. Most Keplerian problems were treated as ideal or under the basic assumptions that the moti...
The effects of the solar radiation pressure and the attraction of the sun and the moon at high Earth...
A theory of an Earth satellite has been developed by considering the Earth's bulge, atmospheric drag...
Many scientific applications require the implementation of satellite formation-flying in various orb...
Through analysis and simulation, previously designed Earth orbiting satellite formations are revisit...
[[abstract]]The linearized dynamic equations used for on-board orbit determination of Sun-synchronou...
The report studies some changes in orbital elements of the artificial satellites of Earth under i...
Abstract The new simulation model of the spacecraft's center of mass motion with taking into ac...
The aim is to create the theory, method, computing program for planning and scientific provision of ...
Application of celestial mechanics to artificial satellite orbit calculations using orbit perturbati...
An analysis is carried out which considers the relationship of orbit mechanics to the satellite navi...
Typescript.Thesis (Ph. D.)--University of Hawaii, 1967.Bibliography: leaves [91]-103.ix, 103 l illus...
The effects of atmosphere drag and zonal harmonics J2 of the gravitational potential of the Cosmos14...
The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orb...
The trajectory analysis of a celestial object orbiting another body is the basis for all other, more...
Abstract. Most Keplerian problems were treated as ideal or under the basic assumptions that the moti...
The effects of the solar radiation pressure and the attraction of the sun and the moon at high Earth...
A theory of an Earth satellite has been developed by considering the Earth's bulge, atmospheric drag...
Many scientific applications require the implementation of satellite formation-flying in various orb...
Through analysis and simulation, previously designed Earth orbiting satellite formations are revisit...
[[abstract]]The linearized dynamic equations used for on-board orbit determination of Sun-synchronou...
The report studies some changes in orbital elements of the artificial satellites of Earth under i...
Abstract The new simulation model of the spacecraft's center of mass motion with taking into ac...
The aim is to create the theory, method, computing program for planning and scientific provision of ...
Application of celestial mechanics to artificial satellite orbit calculations using orbit perturbati...
An analysis is carried out which considers the relationship of orbit mechanics to the satellite navi...
Typescript.Thesis (Ph. D.)--University of Hawaii, 1967.Bibliography: leaves [91]-103.ix, 103 l illus...