Detection aircraft and Mars cruise detection method

A technology of aircraft and Mars, applied in the field of space exploration, can solve the problem of limited walking range of Mars rovers and other patrols, and achieve the effect of flexible planning

Active Publication Date: 2021-03-16
CENT SOUTH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For Mars exploration, although in-situ detection and patrol detection have a high degree of precision, in-situ detection can only be carried out at the landing site, and the walking range of patrol vehicles such as Mars rovers is also quite limited.

Method used

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  • Detection aircraft and Mars cruise detection method
  • Detection aircraft and Mars cruise detection method
  • Detection aircraft and Mars cruise detection method

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Embodiment Construction

[0031] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0032] In the description of the present invention, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc. indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only In order to facilitate the description of the present invention and simplify the description, it does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific ...

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Abstract

The invention discloses a detection aircraft, which comprises a wing, the wing is in a wing shape, the wing is provided with an energy supply system, and the wing is provided with a detection device;the Magnus rotors which are rotationally installed at the front ends of the wings, the Magnus rotors are parallel to the front ends of the wings, and the energy supply system is in transmission connection with the Magnus rotors so as to drive the Magnus rotors to rotate; and a parafoil which is arranged on the upper surface of the wing, and the energy supply system is electrically connected with the parafoil so as to supply energy to the parafoil. According to the detection aircraft, the Magnus rotors are additionally arranged on the front edges of the wings, and in the cruise process, the Magnus rotors can provide larger lift force for the wings in the rotating process; and the Magnus rotor can provide necessary lift force requirements for the Mars probe by taking measures such as changing the rotating speed under the conditions of low density and low dynamic pressure of the external planet atmosphere.

Description

technical field [0001] The invention relates to the field of space detection technology, in particular to a detection aircraft. Background technique [0002] At present, there are three main methods of detecting planets: orbiting detection, in-situ detection and patrolling detection. Surrounding detection is mainly accomplished by means of remote sensing detection by spacecraft orbiting Mars, Venus and other planets. It is easy to observe the details of the surface of Mars very clearly. At the same time, after a satellite observes a certain location, limited by the orbit, it must take a long time to observe the location again, making it difficult to continuously observe some fast-changing phenomena. In-situ detection uses a probe that lands on the surface of a planet to detect rocks, atmosphere or biological information at the position of the probe. Patrol detection is also carried out on the surface of the planet, but because it is carried out by a movable patrol device ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/22B64G1/42
CPCB64G1/105B64G1/22B64G1/42B64G1/1064
Inventor 薛晓鹏徐欣韩凯陈梦洵王泽姜璐璐王嘉麟
Owner CENT SOUTH UNIV
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