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Shane Ross

@RossDynamicsLab • 5,194 subscribers

Engineering math professor at @Virginia_Tech. Dynamics and transport, from spacecraft trajectories to airborne agricultural pathogens.

Shorts

SpaceX wants up to a million satellites as orbital data centers. Half would ride the day-night line, sunlit while the ground below is dark. Top and bottom are the same sky at the same moment. The only difference is how bright they're assumed to be. @SciAm covered it today.

SpaceX wants up to a million satellites as orbital data centers. Half would ride the day-night line, sunlit while the ground below is dark. Top and bottom are the same sky at the same moment. The only difference is how bright they're assumed to be. @SciAm covered it today.

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What if a spacecraft could cycle between Earth and Moon orbits, performing multiple circuits of each, naturally and indefinitely, with zero propulsion? We’ve discovered a new class of stable, prograde, low-energy cycler orbits that do just that. Why these orbits matter: Ballistic → fuel-free Stable → long-term ready Near-chaotic → agile with low ΔV Low-energy → access to Earth/Moon, Lagrange points, Sun–Earth L1/L2, even heliocentric space At the AAS/AIAA Astrodynamics Specialist Conference in Boston next week, I’ll present on a new family of ballistic Earth-Moon cycler orbits that are stable, prograde, and mission agile—unlike any cyclers in the current literature. The example below is shown in both the Earth-Moon rotating frame and inertial frame. Conference Paper:

What if a spacecraft could cycle between Earth and Moon orbits, performing multiple circuits of each, naturally and indefinitely, with zero propulsion? We’ve discovered a new class of stable, prograde, low-energy cycler orbits that do just that. Why these orbits matter: Ballistic → fuel-free Stable → long-term ready Near-chaotic → agile with low ΔV Low-energy → access to Earth/Moon, Lagrange points, Sun–Earth L1/L2, even heliocentric space At the AAS/AIAA Astrodynamics Specialist Conference in Boston next week, I’ll present on a new family of ballistic Earth-Moon cycler orbits that are stable, prograde, and mission agile—unlike any cyclers in the current literature. The example below is shown in both the Earth-Moon rotating frame and inertial frame. Conference Paper:

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Nine families of Earth–Moon cyclers, stable orbits that ferry back and forth between the two, forever. 🌍♾️🌙 In the rotating frame each one closes up and repeats. The label (k₁,k₂) counts the loops: k₁ around the Earth, k₂ around the Moon. Periods run ~42–106 days.

Nine families of Earth–Moon cyclers, stable orbits that ferry back and forth between the two, forever. 🌍♾️🌙 In the rotating frame each one closes up and repeats. The label (k₁,k₂) counts the loops: k₁ around the Earth, k₂ around the Moon. Periods run ~42–106 days.

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Yes, but only for a while. In this simulation, 20 nearly identical pendulums start together, then diverge after a few seconds, the time horizon of predictability. Chaos doesn’t mean randomness, just sensitivity.

Yes, but only for a while. In this simulation, 20 nearly identical pendulums start together, then diverge after a few seconds, the time horizon of predictability. Chaos doesn’t mean randomness, just sensitivity.

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