Spoiler control device, spoiler control method, and storage medium storing thereon program for controlling spoiler

A spoiler control device applicable to an aircraft including left and right spoilers provided on left and right main wings, when driven by an actuator, each spoiler being movable between a basic position positioned on a same plane as a corresponding one of the main wings and a deployed position on a plane tilted relative to the corresponding main wing, the spoiler control device comprising:

• an irregularity detecting unit for detecting whether the left and right spoilers irregularly move toward the deployed position;
• an angle difference determining unit for obtaining angles formed by the left and right spoilers relative to the main wings and determining whether a difference between the obtained angles of the left and right spoilers is equal to or less than a specified value;
• and
• a signal outputting unit for outputting a retracting signal designed to move the left and right spoilers back to the basic position,
• wherein, based on the irregular movement being detected in a given one of the left and right spoilers, the signal outputting unit outputs the retracting signal for the given one of the spoilers and refrains from outputting the retracting signal for the other of the left and right spoilers, and if the difference between the angles of the left and right spoilers becomes equal to or less than the specified value, the signal outputting unit outputs the retracting signal for the other of the left and right spoilers,
• wherein the irregularity detecting unit determines whether the irregular movement of each of the spoilers is caused by irregularity in a position detector configured to detect a position of a rod connected to the spoiler and movable back and forth in a cylinder in the actuator, relative to the cylinder, and
• wherein if the irregular movement of the spoiler is not caused by irregularity in the position detector, the angle difference determining unit obtains, as the angle of the spoiler, the position of the rod and determines whether the difference between the angles of the left and right spoilers is equal to or less than the specified value, and
• wherein, if the irregular movement of the spoiler is caused by irregularity in the position detector, the angle difference determining unit obtains, as the angle of the spoiler, a value detected by an actual measurement sensor configured to detect an actual angle of the spoiler and determines whether the difference between the angles of the left and right spoilers is equal to or less than the specified value.

A spoiler control method applicable to an aircraft including left and right spoilers provided on left and right main wings, when driven by an actuator, each spoiler being movable between a basic position positioned on a same plane as a corresponding one of the main wings and a deployed position on a plane tilted relative to the corresponding main wing, the spoiler control method comprising steps of:

• detecting whether the left and right spoilers irregularly move toward the deployed position;
• obtaining angles formed by the left and right spoilers relative to the main wings and determining whether a difference between the obtained angles of the left and right spoilers is equal to or less than a specified value;
• and
• outputting a retracting signal designed to move the left and right spoilers back to the basic position,
• wherein, based on the irregular movement being detected in a given one of the left and right spoilers, the signal outputting step outputs the retracting signal for the given one of the spoilers and refrains from outputting the retracting signal for the other of the left and right spoilers, and if the difference between the angles of the left and right spoilers becomes equal to or less than the specified value, the signal outputting step outputs the retracting signal for the other of the left and right spoilers.

A non-transitory computer-readable storage medium storing thereon a program for controlling a spoiler, the program being applicable to an aircraft including left and right spoilers provided on left and right main wings, when driven by an actuator, each spoiler being movable between a basic position positioned on a same plane as a corresponding one of the main wings and a deployed position on a plane tilted relative to the corresponding main wing, the program causing a computer to perform steps of:

• detecting whether the left and right spoilers irregularly move toward the deployed position;
• obtaining angles formed by the left and right spoilers relative to the main wings and determining whether a difference between the obtained angles of the left and right spoilers is equal to or less than a specified value;
• and
• outputting a retracting signal designed to move the left and right spoilers back to the basic position,
• wherein, based on the irregular movement being detected in a given one of the left and right spoilers, the signal outputting step outputs the retracting signal for the given one of the spoilers and refrains from outputting the retracting signal for the other of the left and right spoilers, and if the difference between the angles of the left and right spoilers becomes equal to or less than the specified value, the signal outputting step outputs the retracting signal for the other of the left and right spoilers.