Optimal Large-Angle Single-Axis Rotational Maneuvers of Flexible Spacecraft

DOI10.2514/3.56036zbMath0474.49030OpenAlexW1993598227MaRDI QIDQ3930298

James D. Turner, John L. Junkins

Publication date: 1980

Published in: Journal of Guidance and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.56036

zbMATH Keywords

flexible spacecraftnecessary conditionsPontryagin's principletwo-point boundary-value problemclosed-form solution algorithmoptimal large-angle single-axis rotational maneuverssingle-stage relaxation process

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Nonlinear boundary value problems for ordinary differential equations (34B15) Hamilton's equations (70H05) Optimality conditions for problems involving ordinary differential equations (49K15) Motion of the gyroscope (70E05) Generalized coordinates; event, impulse-energy, configuration, state, or phase space for problems in mechanics (70G10)

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