Combined autonomous navigation method of mars exploration approach section
A technology for autonomous navigation and Mars probes, applied in the aerospace field, can solve problems such as inertial influence and error accumulation, and achieve the effect of real-time estimation
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[0016] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.
[0017] Such as Figure 1 to Figure 2 As shown, the present invention provides a kind of combined autonomous navigation method of Mars exploration near section, and it comprises the following steps:
[0018] Step 1, using the on-board solar sensor to measure the line of sight direction of the sun, and using the on-board solar spectrum speed measurement and navigation sensor to measure the relative motion speed of the Mars probe relative to the sun;
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