Reachable Domain for Spacecraft with a Single Impulse

This paper analyzes the reachable domain for spacecraft with a single fixed-magnitude impulse, and overapproximation of the reachable domain is provided for cases involving spacial impulse. A low impulse is assumed, implying elliptical trajectories and a bounded reachable domain. An equation is deve...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2010-05, Vol.33 (3), p.934-942
Hauptverfasser:	Xue, Dan, Li, Junfeng, Baoyin, Hexi, Jiang, Fanghua
Format:	Artikel
Sprache:	eng
Schlagworte:	Constrictions Eccentricity Ellipsoids Elliptical orbits Energy consumption Envelopes Exact sciences and technology Fundamental areas of phenomenology (including applications) Impulses Intersections Mathematical analysis Missions Physics Planes Solid dynamics (ballistics, collision, multibody system, stabilization...) Solid mechanics Spacecraft Trajectories Upper bounds Velocity
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!