Abstract: A rotary connection structure includes a first external connection assembly and a rotation damping structure. The first external connection assembly is for external connection with a first photography device. The rotation damping structure includes a mounting member, a fastening member, and a connecting member. One end of the fastening member extends through the connecting member to fix and connect to the mounting member. The connecting member is rotatable, in a damped manner, about the fastening member. The connecting member is connected to the first external connection assembly. The first external connection assembly can be a clamp assembly. The mounting member is for connection with a second photography device. The second photography device can be a handgrip, and the handgrip is fixedly connected to the mounting member. The rotary connection structure proposed in the present invention realizes rotation of the first photography device and the second photography device.

Abstract: A photography kit is provided, which includes a first photography assembly including a first frame and a clamping assembly including two clamping bodies, a mounting seat, and a first locking assembly. The two clamping bodies are rotatably arranged on two opposite sides of the mounting seat. A connecting part is protruded at outside surfaces of the clamping bodies respectively. An end of the connecting part away from the clamping body is connected with a pressing part, which extends towards a rear end of the mounting seat, so that a pressing space is formed between the pressing part and the mounting seat. The first locking assembly is telescopically mounted to the mounting seat, a limiting part of the first locking assembly extends from the front end of the mounting seat, and the limiting part is configured for being inserted into a positioning hole correspondingly defined on the first frame.

Abstract: A takeoff and landing control method of a multimodal air-ground amphibious vehicle includes: receiving dynamic parameters of the multimodal air-ground amphibious vehicle; processing the dynamic parameters by a coupled dynamic model of the multimodal air-ground amphibious vehicle to obtain dynamic control parameters of the multimodal air-ground amphibious vehicle, wherein the coupled dynamic model of the multimodal air-ground amphibious vehicle comprises a motion equation of the multimodal air-ground amphibious vehicle in a touchdown state; and the motion equation of the multimodal air-ground amphibious vehicle in a touchdown state is determined by a two-degree-of-freedom suspension dynamic equation and a six-degree-of-freedom motion equation of the multimodal air-ground amphibious vehicle in the touchdown state; and controlling takeoff and landing of the multimodal air-ground amphibious vehicle according to the dynamic control parameters of the multimodal air-ground amphibious vehicle.

Abstract: A takeoff and landing control method of a multimodal air-ground amphibious vehicle includes: receiving dynamic parameters of the multimodal air-ground amphibious vehicle; processing the dynamic parameters by a coupled dynamic model of the multimodal air-ground amphibious vehicle to obtain dynamic control parameters of the multimodal air-ground amphibious vehicle, wherein the coupled dynamic model of the multimodal air-ground amphibious vehicle comprises a motion equation of the multimodal air-ground amphibious vehicle in a touchdown state; and the motion equation of the multimodal air-ground amphibious vehicle in a touchdown state is determined by a two-degree-of-freedom suspension dynamic equation and a six-degree-of-freedom motion equation of the multimodal air-ground amphibious vehicle in the touchdown state; and controlling takeoff and landing of the multimodal air-ground amphibious vehicle according to the dynamic control parameters of the multimodal air-ground amphibious vehicle.