Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption

A technology for safe landing and trajectory generation, applied in three-dimensional position/channel control and other directions to achieve the effect of saving fuel consumption

Inactive Publication Date: 2015-01-07
BEIJING INSTITUTE OF TECHNOLOGYGY
View PDF4 Cites 25 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to solve the problem of safe landing in complex terrain areas on Mars, and propose a method for generating safe landing trajectories in complex terrain areas on Mars with the most fuel savings, which can be applied to landing in complex terrain areas on Mars, and can save power while avoiding obstacles. fuel consumption

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption
  • Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption
  • Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0052] In order to better illustrate the purpose and advantages of the present invention, the content of the present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0053] The present invention first establishes a navigation function according to the obstacle terrain, and solves the control force through the navigation function, which can effectively avoid the collision between the lander and the obstacle, and land safely to the target landing point. Secondly, the solved control force is introduced into the dynamic equation of Mars power descent, so that part of the control force is used to achieve obstacle avoidance. At this time, optimizing the landing trajectory of the modified dynamic equation can not only ensure that the landing process can effectively avoid obstacles but also reduce fuel consumption. Concrete flow process of the present invention is as figure 1 shown, including the following steps:

[0054] 1) ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention relates to a Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption, and belongs to the technical field of planet landing. The method comprises the steps that a Mars powered lowering kinetic model is built at first, a navigation function is built according to the target landing terrain, obstacle avoidance control force obtained through the navigation function can effectively avoid collision between a lander and an obstacle, and the lander is safely landed to a target landing point. According to the Mars complex terrain region safe landing trajectory generation method with minimum fuel consumption, the obtained obstacle avoidance control force is introduced into a Mars powered lowering kinetic equation, the control force is partially used for achieving obstacle avoidance, and landing trajectory optimization is carried out on the improved kinetic equation, so that obstacle avoidance is achieved, and meanwhile fuel consumed by the powered lowering trajectory is saved. The Mars complex terrain region safe landing trajectory generation method can not only take the target landing area terrain into consideration, but also effectively reduce fuel consumption, and overcomes the defects that obstacle avoidance cannot be achieved and fuel consumption is large in traditional optimization trajectory and obstacle avoidance.

Description

technical field [0001] The invention relates to a method for generating safe landing trajectories in complex terrain areas of Mars with the least fuel, and belongs to the technical field of planetary landings. Background technique [0002] With the continuous development of human society and economy and the continuous advancement of science and technology, Mars exploration has become one of the hotspots of deep space exploration. Among them, the Mars landing exploration mission is the most scientifically meaningful and challenging. Since complex terrain areas on Mars have higher scientific exploration value, in order to achieve breakthrough scientific results, future landers need to have the ability to land in complex terrain areas. In order to reduce the fuel consumption during the powered descent and reduce the mission cost, it is very necessary to study the fuel-optimized landing trajectory. [0003] At present, during the powered descent of Mars, researches have been ca...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 崔平远胡海静朱圣英高艾徐瑞
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products