Fuel-Optimal Transfers Between Coplanar Circular Orbits Using Variable-Specific-Impulse Engines

Minimum fuel circular-to-circular low-thrust orbital transfers with prescribed transfer time and with the thrust always directed parallel to the velocity vector are developed for a variable-specific-impulse system. The changeable specific impulse serves as the control variable. The power input is as...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2005-07, Vol.28 (4), p.795-800
Hauptverfasser:	Seywald, Hans, Roithmayr, Carlos M, Troutman, Patrick A, Park, Sang-Young
Format:	Artikel
Sprache:	eng
Schlagworte:	Applied sciences Circular orbits Computer science control theory systems Control theory. Systems Exact sciences and technology Fundamental areas of phenomenology (including applications) Miscellaneous Orbits Physics Plasma Solid dynamics (ballistics, collision, multibody system, stabilization...) Solid mechanics Velocity
Online-Zugang:	Volltext
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