Descripción
|
|
---|---|
The problem of optimal impulsive collision avoidance between two colliding objects in 3-dimensional elliptical Keplerian orbits is investigated with the purpose of establishing the optimal impulse direction and orbit location that give rise to the maximum miss distance following the maneuver. Closed-form analytical expressions are provided that predicts such distance and can be employed to perform a full optimization analysis. After verifying the accuracy of the expression for any orbital eccentricity and encounter geometry the optimum maneuver direction is derived as a function of the arc length separation between the maneuver point and the predicted collision point. The provided formulas can be used for high accuracy instantaneous estimation of the outcome of a generic impulsive collision avoidance maneuver and its optimization. | |
Internacional
|
Si |
Nombre congreso
|
23rd AAS/AIAA SpaceFlight Mechanics Meeting |
Tipo de participación
|
960 |
Lugar del congreso
|
Kauai, Hawaii |
Revisores
|
Si |
ISBN o ISSN
|
ISSN 1081-6003 |
DOI
|
|
Fecha inicio congreso
|
10/02/2013 |
Fecha fin congreso
|
14/02/2013 |
Desde la página
|
1 |
Hasta la página
|
17 |
Título de las actas
|
Advances in the Astronautical Sciences Series, Vol 148 |