Guidance trajectories for spacecraft rendezvous

DOI10.1007/s10957-007-9165-5zbMath1176.70035OpenAlexW2079581687MaRDI QIDQ946320

M. W. Weeks, M. Ciarcià, Angelo Miele

Publication date: 23 September 2008

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10957-007-9165-5

zbMATH Keywords

optimal controlcalculus of variationsrendezvousguidancespace trajectoriesBolza problemsMayer problemsmultiple-subarc sequential gradient-restoration algorithmtransformation techniques

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (4)

Optimal starting conditions for the rendezvous maneuver. I: Optimal control approach ⋮ Optimal starting conditions for the rendezvous maneuver. II: Mathematical programming approach ⋮ Optimal trajectories for spacecraft rendezvous ⋮ On impulsive hyperbolic differential inclusions with nonlocal initial conditions

Cites Work

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• Lower-order penalization approach to nonlinear semidefinite programming
• Recent advances in gradient algorithms for optimal control problems
• Sequential gradient-restoration algorithm for optimal control problems with general boundary conditions
• Multiple-subarc gradient-restoration algorithm. I: Algorithm structure
• Multiple-subarc gradient-restoration algorithm. II: Application to a multistage launch vehicle design
• Linearized impulsive rendezvous problem
• Method of particular solutions for linear, two-point boundary-value problems
• Sequential gradient-restoration algorithm for optimal control problems
• Summary and comparison of several gradient-restoration algorithms for optimal control problems
• Optimal multiple-impulse time-fixed rendezvous between circular orbits
• Fuel-optimal rendezvous near a point in general Keplerian orbit
• Primer vector theory applied to the linear relative-motion equations
• Optimal power-limited rendezvous with upper and lower bounds on thrust
• Primer vector on fixed-time impulsive trajectories.

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