Pages that link to "Item:Q880947"
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The following pages link to Approximate analysis for relative motion of satellite formation flying in elliptical orbits (Q880947):
Displaying 16 items.
- The equations of relative motion in the orbital reference frame (Q285132) (← links)
- Study on relative orbital configuration in satellite formation flying (Q608580) (← links)
- Solution set on the natural satellite formation orbits under first-order Earth's non-spherical perturbation (Q608662) (← links)
- Modeling orbital relative motion to enable formation design from application requirements (Q642301) (← links)
- The relative motion of earth orbiting satellites (Q815668) (← links)
- Invariant relative orbits for satellite constellations: a second-order theory (Q945334) (← links)
- Useful relative motion description method for perturbations analysis in satellite formation flying (Q957648) (← links)
- Effects of interplanetary dust on the LISA drag-free constellation (Q990335) (← links)
- Comparison of two methods in satellite formation flying (Q1430600) (← links)
- Semianalytical solutions of relative motions with applications to periodic orbits about a nominal circular orbit (Q1720880) (← links)
- An in-plane \(J_2\)-invariance condition and control algorithm for highly elliptical satellite formations (Q2033671) (← links)
- Mathematical modeling and simulation of nonlinear spacecraft rendezvous and formation flying problems via averaging method (Q2219610) (← links)
- Frozen-anomaly transformation for the elliptic rendezvous problem (Q2348885) (← links)
- Improved initialization conditions and single impulsive maneuvers for \(J_2\)-invariant relative orbits (Q2348896) (← links)
- Aerial monitoring of slow moving convoys using elliptical orbits (Q2415106) (← links)
- An analytic method to determine future close approaches between satellites (Q3680344) (← links)
