Optimal trajectories for spacecraft rendezvous

DOI10.1007/s10957-007-9166-4zbMath1176.70036OpenAlexW2020723852MaRDI QIDQ946319

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/s10957-007-9166-4

zbMATH Keywords

optimal controlcalculus of variationsrendezvousspace trajectoriesBolza problemsMayer problemssequential 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 (7)

Operations research in the space industry ⋮ Optimal starting conditions for the rendezvous maneuver. I: Optimal control approach ⋮ Optimal starting conditions for the rendezvous maneuver. II: Mathematical programming approach ⋮ Model Predictive Control approach for guidance of spacecraft rendezvous and proximity maneuvering ⋮ On impulsive hyperbolic differential inclusions with nonlocal initial conditions ⋮ Low-thrust transfers to southern \(L_2\) near-rectilinear halo orbits facilitated by invariant manifolds ⋮ STOCHASTIC MODEL PREDICTIVE CONTROL FOR SPACECRAFT RENDEZVOUS AND DOCKING VIA A DISTRIBUTIONALLY ROBUST OPTIMIZATION APPROACH

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• Optimal power-limited rendezvous with upper and lower bounds on thrust
• Primer vector on fixed-time impulsive trajectories.

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