An aircraft rudder pedal includes a frame, a pair of pedals, an output shaft and a mechanical kinematic chain for transmitting to the output shaft a displacement of at least one of the pedals relative to the frame. The mechanical kinematic chain comprises a central transmission part able to be rotated relative to the frame by a displacement of one of the pedals relative to the frame. The mechanical kinematic chain also includes a transmission mechanism joining the central transmission part to the output shaft. The transmission mechanism includes a homokinetic association of two universal joints between said central transmission part and the output shaft.

An aircraft rudder pedal comprising a frame and at least one pedal side system. The or each pedal side system includes a pedal and an articulated support structure of the pedal connecting the pedal to the frame. The articulated support structure of said pedal comprises a crank, a lever and a support link. The crank presents a first pivotal articulation connection to the frame and a second pivotal articulation connection with the support link. The lever presents a first pivotal articulation connection with the frame and a second pivotal articulation connection with the support link.

To provide an aircraft of which flight efficiency can be improved. An image capturing method according to this embodiment is a method for capturing an image of an object to be photographed by using a plurality of aircrafts including an image capturing part. The image capturing method includes a ranking step of setting up a predetermined ranking for each of the aircrafts, a control step of performing control on the basis of the ranking, and an image capturing step of moving the aircraft and using the image capturing part to capture an image of the object. According to this configuration, a plurality of aircrafts can be used to capture images of a plurality of objects to be photographed simultaneously from different angles.

To provide an aircraft of which flight efficiency can be improved. An image capturing method according to this embodiment is a method for capturing an image of an object to be photographed by using a plurality of aircrafts including an image capturing part. The image capturing method includes a ranking step of setting up a predetermined ranking for each of the aircrafts, a control step of performing control on the basis of the ranking, and an image capturing step of moving the aircraft and using the image capturing part to capture an image of the object. According to this configuration, a plurality of aircrafts can be used to capture images of a plurality of objects to be photographed simultaneously from different angles.

An airplane rudder and brake pedal assembly includes a rudder arm assembly having one rudder arm with first upper and lower arm portions, and another rudder arm with second upper and lower arm portions. The rudder arm assembly is assembled to a beam at an intersection of the first upper and lower arm portions, and an intersection of the second upper and lower arm portions. The first and second rudder arms are configured to rotate about the beam at the intersection. The rotation of the first and second rudder arms is configured to adjust control surfaces that control a yaw axis of the airplane. A brake pedal is attached to the first and second lower arm portions. Rotation of the brake pedal brakes the airplane. A rotary sensor is assembled to the brake pedal and the lower arm portion, and configured to determine an extent of the brake pedal rotation.

Disclosed herein is a monobloc and removable pedal module for an aircraft rudder bar. The pedal module, which is intended for a rudder bar, includes a pedal, at least one integrated adjustment system, and a connection device which enables a removable connection of the pedal module to be produced. The pedal module is a monobloc component in order to simplify and facilitate its replacement via the removable connection obtained by the connection device.

Disclosed herein is a monobloc and removable pedal module for an aircraft rudder bar. The pedal module, which is intended for a rudder bar, includes a pedal, at least one integrated adjustment system, and a connection device which enables a removable connection of the pedal module to be produced. The pedal module is a monobloc component in order to simplify and facilitate its replacement via the removable connection obtained by the connection device.

To provide an aircraft of which flight efficiency can be improved. An image capturing method according to this embodiment is a method for capturing an image of an object to be photographed by using a plurality of aircrafts including an image capturing part. The image capturing method includes a ranking step of setting up a predetermined ranking for each of the aircrafts, a control step of performing control on the basis of the ranking, and an image capturing step of moving the aircraft and using the image capturing part to capture an image of the object. According to this configuration, a plurality of aircrafts can be used to capture images of a plurality of objects to be photographed simultaneously from different angles.

To provide an aircraft of which flight efficiency can be improved. An image capturing method according to this embodiment is a method for capturing an image of an object to be photographed by using a plurality of aircrafts including an image capturing part. The image capturing method includes a ranking step of setting up a predetermined ranking for each of the aircrafts, a control step of performing control on the basis of the ranking, and an image capturing step of moving the aircraft and using the image capturing part to capture an image of the object. According to this configuration, a plurality of aircrafts can be used to capture images of a plurality of objects to be photographed simultaneously from different angles.

An airplane rudder and brake pedal assembly includes a rudder arm assembly having one rudder arm with first upper and lower arm portions, and another rudder arm with second upper and lower arm portions. The rudder arm assembly is assembled to a beam at an intersection of the first upper and lower arm portions, and an intersection of the second upper and lower arm portions. The first and second rudder arms are configured to rotate about the beam at the intersection. The rotation of the first and second rudder arms is configured to adjust control surfaces that control a yaw axis of the airplane. A brake pedal is attached to the first and second lower arm portions. Rotation of the brake pedal brakes the airplane. A rotary sensor is assembled to the brake pedal and the lower arm portion, and configured to determine an extent of the brake pedal rotation.