Method for evaluating compatibility between low-orbit navigation system and medium-high orbit navigation system
A navigation system, medium and high orbit technology, applied in the field of satellite navigation and positioning, can solve the problems of high transmission power, deviation, and the influence of Doppler frequency shift on spectrum separation coefficient is not considered, and achieves equivalent carrier-to-noise ratio attenuation, The effect of reducing bias
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0052] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present invention.
[0053] like figure 1 As shown, the present invention relates to a compatibility evaluation method between a low-orbit navigation system and a middle-high orbit navigation system, comprising the following steps:
[0054] Step 1. Establish a system scenario through MATLAB and STK software, including generating a low-orbit navigation (LEO) satellite constellation, a medium-high orbit navigation system (Glonass) satellite constellation, and establishing a ground navigation receiver. The specific steps are:
[0055] Step 101: Combine MA...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


