Control and navigation of artificial earth satellites in nearly circular orbits
Abstract
The generation of ballistic-support techniques for satellites in nearly circular orbits are examined. Particular emphasis is placed on the development of mathematical models of motion and perturbation, as well as on orbit determination and the planning of navigation-system operations. Consideration is given to aspects of the control of individual satellites as well as satellite systems.
- Publication:
-
Moscow Izdatel Mashinostroenie
- Pub Date:
- 1988
- Bibcode:
- 1988MIzMa.........R
- Keywords:
-
- Circular Orbits;
- Earth Orbits;
- Satellite Control;
- Satellite Perturbation;
- Space Navigation;
- Ballistics;
- Geopotential;
- Gravitational Effects;
- Heuristic Methods;
- High Thrust;
- Least Squares Method;
- Mathematical Models;
- Optimal Control;
- Orbit Perturbation;
- Orbital Elements;
- Potential Theory;
- Satellite Orbits;
- State Vectors;
- Stochastic Processes;
- Three Body Problem;
- Space Communications, Spacecraft Communications, Command and Tracking