Pages that link to "Item:Q5943545"

The following pages link to \(J_2\) invariant relative orbits for spacecraft formations (Q5943545):

Displaying 29 items.

• Solution set on the natural satellite formation orbits under first-order Earth's non-spherical perturbation (Q608662) (← links)
• \(J _{2}\) invariant relative orbits via differential correction algorithm (Q612443) (← links)
• Modeling orbital relative motion to enable formation design from application requirements (Q642301) (← links)
• Canonical modelling of relative spacecraft motion via epicyclic orbital elements (Q816892) (← links)
• Invariant relative orbits for satellite constellations: a second-order theory (Q945334) (← links)
• Relative motion of satellites exploiting the super-integrability of Kepler's problem (Q968345) (← links)
• A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary (Q1637799) (← links)
• Symmetry properties of optimal relative orbit trajectories (Q1665243) (← links)
• A simple time domain collocation method to precisely search for the periodic orbits of satellite relative motion (Q1719255) (← links)
• Analysis of \(J_2\)-perturbed motion using mean non-osculating orbital elements (Q1766280) (← links)
• Bounded relative motions for formation flying in displaced orbits by low-thrust propulsion (Q1785914) (← links)
• Application of Hamiltonian structure-preserving control to formation flying on a \(J_2\)-perturbed mean circular orbit (Q1955973) (← links)
• Bounded motion design in the Earth zonal problem using differential algebra based normal form methods (Q2004685) (← links)
• Semi-analytical model for third-body perturbations including the inclination and eccentricity of the perturbing body (Q2005629) (← links)
• Long-term evolution of orbital inclination due to third-body inclination (Q2033666) (← links)
• An in-plane \(J_2\)-invariance condition and control algorithm for highly elliptical satellite formations (Q2033671) (← links)
• Reducing inter-satellite drift of low Earth orbit constellations using short-periodic corrections (Q2034093) (← links)
• Bounded Martian satellite relative motion (Q2049216) (← links)
• Nonsingular vectorial reformulation of the short-period corrections in Kozai's oblateness solution (Q2138488) (← links)
• Nonlinear analytic solution for perturbed relative motion using differential equinoctial elements (Q2203829) (← links)
• Improved initialization conditions and single impulsive maneuvers for \(J_2\)-invariant relative orbits (Q2348896) (← links)
• Long-term passive distance-bounded relative motion in the presence of \(J_2\) perturbations (Q2348911) (← links)
• Bounded relative motion under zonal harmonics perturbations (Q2359250) (← links)
• Integrable approximation of \(J_2\)-perturbed relative orbits (Q2375760) (← links)
• Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations (Q2376779) (← links)
• The \(J_2\) invariant relative configuration of spaceborne SAR interferometer for digital elevation measurement (Q2393514) (← links)
• Modelling natural formations of LEO satellites (Q2458482) (← links)
• Relative orbit design and control of formation around displaced solar orbits (Q2853489) (← links)
• Сравнение моделей относительного движения группы космических аппаратов (Q5089849) (← links)