A spacecraft includes: an ejector that ejects an object being a base of a shooting star at a speed of 120 m/s or more; a direction controller that controls a direction in which the object is ejected; and a position controller that controls a position at which the object is ejected. The ejector sequentially ejects objects at a predetermined time interval. The ejector controls a time interval individually for each of the objects. The spacecraft includes an autonomous controller that autonomously controls the ejector, direction controller, and position controller, to eject the object in a predetermined ejecting direction and at predetermined ejecting position and speed. The autonomous controller controls ejection of the object based on a result of determination on measurement data individually performed by each of arithmetic units.
SPACECRAFT, ARTIFICIAL SHOOTING STAR GENERATION METHOD, AND SERVICE PROVISION METHOD
2022-02-10
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
SPACECRAFT, ARTIFICIAL SHOOTING STAR GENERATION METHOD, AND SERVICE PROVISION METHOD
Europäisches Patentamt | 2022
|SPACE CRAFT, ARTIFICIAL SHOOTING STAR GENERATING METHOD, AND SERVICE PROVIDING METHOD
Europäisches Patentamt | 2020
|Engineering Index Backfile | 1945
|Shooting Star - Mercedes CLS Shooting Brake
Kraftfahrwesen | 2012
|