Nonlinear model predictive control strategy for low thrust spacecraft missions

DOI10.1002/oca.2049zbMath1284.93101OpenAlexW1912128555MaRDI QIDQ5408034

Joseph A. Starek, Ilya V. Kolmanovsky

Publication date: 8 April 2014

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2027.42/102723

zbMATH Keywords

spacecraftrendezvousmodel predictive controltrajectory optimizationlow thrust

Mathematics Subject Classification ID

Related Items (1)

Field programmable gate array based predictive control system for spacecraft rendezvous in elliptical orbits

Cites Work

• Radially accelerated optimal feedback orbits in central gravity field with linear drag
• Constrained model predictive control: Stability and optimality
• Nonlinear Model Predictive Control: An Introductory Review
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