Attitude control apparatus, flying object, and attitude control method
AssigneeCanon Kabushiki Kaisha
InventorHIROTAKA SHINDO
Life of this patent
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Abstract
An attitude control apparatus included in a flying object configured to generate thrust in accordance with a control amount. The attitude control apparatus includes a movable unit that is movable relative to a body of the flying object, a drive unit configured to move the movable unit and a processor configured to output the control amount for restoring an attitude of the body when the attitude has changed and to control the drive unit to move the movable unit in a direction to restore the attitude.
Claims14
An attitude control apparatus included in a flying object configured to generate thrust in accordance with a control amount, the attitude control apparatus comprising:
- a movable unit that is movable relative to a body of the flying object;
- a drive unit configured to move the movable unit;
- and
- a processor configured to output the control amount for restoring an attitude of the body when the attitude has changed and to control the drive unit to move the movable unit in a direction to restore the attitude.
A flying object comprising:
- an attitude control apparatus configured to generate thrust in accordance with a control amount;
- and
- a body,
- wherein the attitude control apparatus includes:
- a movable unit capable of moving relative to a body of the flying object;
- a drive unit configured to move the movable unit;
- and
- a processor configured to output the control amount for restoring an attitude of the body when the attitude has changed and control the drive unit to move the movable unit in a direction to restore the attitude.
An attitude control method comprising:
- controlling an attitude of a flying object configured to generate thrust in accordance with a control amount;
- and
- moving a movable unit relative to a body of the flying object,
- wherein when an attitude of the body has changed, the control amount for restoring the attitude is output and the movable unit is moved in a direction to restore the attitude.
Dependencies are inferred from the claim text.