The present invention provides a means by which heat generated in an airtight container for a flying object flying at high altitude can be exhausted to the outside. Container 12 is a cabin of a gas balloon and comprises Main Body 121, which is an airtight container for accommodating Crew Member H1 and is filled with Air 122, Heat Transfer Member 125 made of a material that has a high thermal conductivity such as aluminum and that covers the inside of Main Body 121 and is partially in contact with Heat Absorber Holder 123, Heat Absorber Holder 123 that is a container made of a material that has a high thermal conductivity, such as aluminum, and is located outside of Main Body 121, and Heat Absorber 124 contained in Heat Absorber Holder 123. Heat generated by Crew Member H1 is transferred via Air 122 to Heat Transfer Member 125 and then to Heat Absorber Holder 123. Heat Absorber 124 absorbs heat from Heat Absorber Holder 123 as heat of vaporization and changes from a liquid to a gas.

Disclosed is an electronic gimbal with camera and mounting configuration. The gimbal can include an inertial measurement unit which can sense the orientation of the camera and three electronic motors which can manipulate the orientation of the camera. The gimbal can be removably coupled to a variety of mount platforms, such as an aerial vehicle, a handheld grip, or a rotating platform. Moreover, a camera can be removably coupled to the gimbal and can be held in a removable camera frame. Also disclosed is a system for allowing the platform, to which the gimbal is mounted, to control settings of the camera or to trigger actions on the camera, such as taking a picture, or initiating the recording of a video. The gimbal can also provide a connection between the camera and the mount platform, such that the mount platform receives images and video content from the camera.

A control device mounted in a first mobile body that includes a camera and an antenna includes: the camera configured to operate such that a direction of an optical axis of the camera and an oriented direction of the antenna are linked to each other; an identification unit configured to identify a second mobile body through image recognition from a captured image captured by the camera operating; and an antenna control unit configured to control the oriented direction of the antenna such that a position of the identified second mobile body in the captured image is a predetermined position.

A guidance system for a missile performs a method for guiding the missile. The guidance system includes a target detector and a window between a target and the target detector. The window including a first pane, a second pane and a channel between the first pane from the second pane. Radiation from the target passes through the window including the first pane, the second pane and the channel to be detected at the target detector. A gas is transported through the channel between the first pane and the second pane to control a temperature of the window.

To provide a system, a method and the like for acquiring more images or more quickly focused images. A control device acquires information regarding a situation of a range captured by an imaging device, determines a mode according to an assumed situation of the range captured by the imaging device among a plurality of focusing modes, and transmits designation information specifying the determined mode to the imaging device. The imaging device receives the designation information from the control device, and captures an image using the mode specified by the received designation information.

To provide an electronic component capable of performing attitude control of an aircraft in an ex-post manner. An electronic component according to the present disclosure is attachable to an aircraft. The electronic component includes an arm part, an attachment part for attaching to the main body part of the aircraft, and a connecting part for connecting the arm part and the attachment part so that the arm part and the attachment part can be displaced within a predetermined range. The connecting part is connected to a position that coincides with or substantially coincides with the center of gravity of the arm part. Further, when attached to the aircraft, the connecting part coincides with or substantially coincides with the lift generating center of the aircraft.

[Object] To provide a control device which enables a flight vehicle device to obtain a highly precise image.

[Solution] Provided is the control device including an illuminating control unit configured to adjust a light amount of an illuminating device according to an inclination of a fuselage of a flight vehicle device that has an imaging device configured to photograph a photographing target and the illuminating device configured to illuminate the photographing target.

Embodiments of the present invention is a shock-absorbing bracket, including: a mounting bracket; a base, where the base is spaced apart from the mounting bracket; and a plurality of shock-absorbing elements, where one end of each of the plurality of shock-absorbing elements is connected with the mounting bracket. Through the structure, the mounting bracket and the base form a triangular shock-absorbing mounting structure in a vertical direction, the stability of the shock-absorbing bracket is improved, and the shock-absorbing effect is good.

A control method applied to a photographing apparatus that includes a lens, an external device, and a body communicatively connected to the lens and the external device. The control method includes the body sending a shutter opening command to the lens; the lens sending a trigger signal to the body according to the shutter opening command, the trigger signal including a first pulse and a second pulse; and the body receiving the trigger signal sent from the lens, triggering a resetting operation of an image sensor inside the body according to the first pulse and triggering activation of the external device according to the second pulse.

A gimbal photographing device includes a fuselage; a folding mechanism, connected to the fuselage; and a gimbal camera, connected to the folding mechanism. The gimbal camera is foldable and unfoldable relative to the fuselage via the folding mechanism. A power switch is disposed on the fuselage. The folding mechanism includes a base connected to the gimbal camera. When the gimbal camera is unfolded relative to the fuselage, the base is configured to abut against the power switch to turn on the gimbal photographing device.