Closed-form solution of an idealized, optimal, highly eccentric hyperbolic rendezvous problem

DOI10.1007/BF02169490zbMath0851.70020MaRDI QIDQ1918359

Thomas E. Carter

Publication date: 31 July 1996

Published in: Dynamics and Control (Search for Journal in Brave)

Mathematics Subject Classification ID

Dynamics of a system of particles, including celestial mechanics (70F99) Orbital mechanics (70M20)

Related Items (1)

The theory of asynchronous relative motion. II: Universal and regular solutions

Cites Work

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• Optimal impulsive space trajectories based on linear equations
• Linearized impulsive rendezvous problem
• New form for the optimal rendezvous equations near a Keplerian orbit
• Fuel-optimal rendezvous near a point in general Keplerian orbit
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• Primer vector on fixed-time impulsive trajectories.
• Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.
• An efficient method for calculating optimal free-space n-impulse trajectories.
• Optimal two- and three-impulse fixed-time rendezvous in the vicinityof a circular orbit

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