http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114611274-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a4d153f0fbb82a77147c3f244aec9f0c |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G06F30-20 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G06F30-20 |
| filingDate | 2022-02-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c54c866faa8b2a2a11885a82e4e101cd http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1a0c73d35659a384a7bf45a4d4db6f98 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2f78d38d7c06d48a428ae096fba64988 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c3b3338a3a1eb6e7b2189db54b7f2cbf http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b8ad979cbde4c38c70ad7e797ba4a4a3 |
| publicationDate | 2022-06-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-114611274-A |
| titleOfInvention | A calculation method for the evolution of the inclination vector of the debris in the geosynchronous orbit |
| abstract | The method for calculating the evolution of the inclination angle vector of geosynchronous orbit debris disclosed in the present invention includes first calculating the influence of the main term J2 of the earth's aspheric perturbation on the change rate of the inclination debris, and calculating the angular frequency and precession of the inclination vector of the synchronous orbit debris under the influence of the J2 term. Then calculate the frequency, precession period and angular rate of the geosynchronous orbit debris inclination vector caused by solar gravity and lunar gravity respectively; and the angular rate of precession for a composite calculation. The method for calculating the evolution of the inclination angle vector of the geosynchronous orbit debris of the present invention separately calculates the effects of the J2 term of the earth and the gravitational force of the sun and the moon. It is fast and can be used to analyze and calculate the long-term evolution of the geosynchronous orbit debris orbit. |
| priorityDate | 2022-02-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419556976 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID866 |
Total number of triples: 17.