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A method for detection aircraft and Mars cruising detection

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: 2022-06-24
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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  • A method for detection aircraft and Mars cruising detection
  • A method for detection aircraft and Mars cruising detection
  • A method for detection aircraft and Mars cruising detection

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Embodiment Construction

[0031] The following describes in detail the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary, only used to explain the present invention, and should not be construed as a limitation of the present invention.

[0032] In the description of the present invention, it should be understood that the orientations related to the description, such as up, down, front, rear, left, right, etc., are based on the orientation or positional relationship shown in the drawings, and are only In order to facilitate the description of the present invention and simplify the description, it is not indicated or implied that the indicated device or element must have a particular orientation, be constructed and operate...

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Abstract

The invention discloses a detection aircraft, comprising: a wing, the wing is an airfoil, the wing is provided with an energy supply system, and a detection device is provided on the wing; a Magnus rotor, the The Magnus rotor is rotatably installed on the front end of the wing, and the Magnus rotor is arranged parallel to the front end of the wing, and the energy supply system is connected with the Magnus rotor to drive the The Magnus rotor rotates; the parafoil is arranged on the upper surface of the wing, and the energy supply system is electrically connected with the parafoil to supply energy to the parafoil. This application detects that the Magnus rotor is installed on the leading edge of the wing. During the cruising process, the Magnus rotor can provide greater lift for the wing during the rotation process, and the Magnus rotor Under the low density and low dynamic pressure conditions of the outer planetary atmosphere, it can provide the necessary lift demand for the Mars probe by changing the rotation speed and other measures.

Description

technical field [0001] The invention relates to the technical field of space exploration, in particular to a detection aircraft. Background technique [0002] At present, the detection methods of planets mainly include orbital detection, in-situ detection and patrol detection. Surrounding detection is mainly accomplished by means of remote sensing detection by spacecraft operating in orbits around other planets such as Mars and Venus. For example, the distance between probes orbiting Mars and the surface of Mars is generally more than a few hundred kilometers. It is easy to observe the details of the Martian surface very clearly. At the same time, after a satellite observes a certain location once, due to the limitation of the operating orbit, the location must be observed again after a long interval, and it is difficult to continuously observe some rapidly changing phenomena. On the other hand, in-situ detection uses a probe that has landed on the surface of a planet to d...

Claims

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Application Information

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Patent Type & Authority Patents(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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