Method for measuring latitude and longitude of fire point sensor
A determination method and sensor technology are applied in the field of satellite attitude control to achieve the effect of improving intelligence and improving practicability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0052] 1. Known fire sensor installation matrix C throughout the star PBfire =[0,1,0;-1,0,0;0,0,1] and installation position
[0053] 2. When t=1000.125 seconds, the sensor outputs the fire point moment t_fire=1000.125, and the orientation unit vector of the fire point in the reference mirror coordinate system of the sensor is u p =[0.037007109559268 0.0370071095592680.998629534754574] T ;
[0054] 3. Determine the satellite attitude matrix C corresponding to the time t_fire by looking up the table BO_fire =[0.99999999948125828,1.2893420485576845e-005,-2.9516826041131594e-005;-1.2893922240783673e-005,0.99999999977239318,-1.6998827341560552e-005;2.9516606861290651e-005,1.6999207920420645e-005,0.99999999941989848];
[0055] 4. Satellite orbit position at time t_fire [x_fire y_fire z_fire] T =[-4285.8020078297141, 1631.1533849416005, -5124.1037730588559] T and the transformation matrix C of the satellite from the J2000 inertial coordinate system to the satellite orbital co...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com