Trajectory Optimization Using Nonsingular Orbital Elements and True Longitude

The system and adjoint differential equations needed to solve low-thrust transfer and rendezvous trajectories are derived in terms of nonsingular orbit elements, with the true longitude selected as the sixth variable that also defines the radial distance. The perturbation accelerations are resolved...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 1997-09, Vol.20 (5), p.1003-1009
1. Verfasser:	Kechichian, Jean Albert
Format:	Artikel
Sprache:	eng
Schlagworte:	Optimization Orbital elements Trajectory optimization Variables
Online-Zugang:	Volltext
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