The following pages link to (Q5384932):
Displaying 12 items.
- A study of single- and double-averaged second-order models to evaluate third-body perturbation considering elliptic orbits for the perturbing body (Q460370) (← links)
- Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations (Q473630) (← links)
- Some orbital characteristics of lunar artificial satellites (Q642412) (← links)
- Analytical theory of a lunar artificial satellite with third body perturbations (Q850706) (← links)
- Third-body perturbation using a single averaged model: application in nonsingular variables (Q936231) (← links)
- Third-body perturbation in the case of elliptic orbits for the disturbing body (Q955953) (← links)
- Semianalytic integration of high-altitude orbits under lunisolar effects (Q1955051) (← links)
- Inner third-body perturbations (Q2004764) (← links)
- Semi-analytical model for third-body perturbations including the inclination and eccentricity of the perturbing body (Q2005629) (← links)
- A study of the errors of the averaged models in the restricted three-body problem in a short time scale (Q2516812) (← links)
- Single-averaged model for analysis of frozen orbits around planets and moons (Q2675565) (← links)
- Long-term evaluation of orbital dynamics in the Sun-planet system considering axial-tilt (Q4643600) (← links)
