Title:
【発明の名称】人工衛星の軌道制御方式
Document Type and Number:
Japanese Patent JP2518212
Kind Code:
B2
Abstract:
A system for controlling the orbit of a satellite by operating a plurality of thrusters as required senses an actual attitude of the satellite, compares an evaluation value set up on the basis of the sensed attitude with a threshold which is adequately changing, and ON-OFF controls the firing the thruster based on the relationship between the evaluation value and the threshold.
Inventors:
KATSU TAKAKAZU
OGURA NAOTO
OGURA NAOTO
Application Number:
JP15022186A
Publication Date:
July 24, 1996
Filing Date:
June 26, 1986
Export Citation:
Assignee:
NIPPON ELECTRIC CO
International Classes:
G05D1/08; B64G1/26; (IPC1-7): B64G1/26
Domestic Patent References:
| JP6146798A |
Attorney, Agent or Firm:
Hachiman Yoshihiro