Pages that link to "Item:Q2375760"
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The following pages link to Integrable approximation of \(J_2\)-perturbed relative orbits (Q2375760):
Displaying 13 items.
- Satellite onboard orbit propagation using Deprit's radial intermediary (Q469052) (← links)
- \(J _{2}\) invariant relative orbits via differential correction algorithm (Q612443) (← links)
- Variational and symplectic integrators for satellite relative orbit propagation including drag (Q724676) (← links)
- Second-order state transition for relative motion near perturbed, elliptic orbits (Q861360) (← links)
- A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary (Q1637799) (← links)
- Fourier series approximations to \(J_2\)-bounded equatorial orbits (Q1718669) (← links)
- A new radial, natural, higher-order intermediary of the main problem four decades after the elimination of the parallax (Q2005647) (← links)
- An in-plane \(J_2\)-invariance condition and control algorithm for highly elliptical satellite formations (Q2033671) (← links)
- Long-term passive distance-bounded relative motion in the presence of \(J_2\) perturbations (Q2348911) (← links)
- First-order analytic propagation of satellites in the exponential atmosphere of an oblate planet (Q2359248) (← links)
- Bounded relative motion under zonal harmonics perturbations (Q2359250) (← links)
- Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations (Q2376779) (← links)
- The triaxiality role in the spin-orbit dynamics of a rigid body (Q2690583) (← links)
