http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112464359-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5ba80bcae1f37d9d779906b19ae0dd95 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G06F2119-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T90-00 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G06F30-15 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G06F30-28 |
| classificationIPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G06F119-14 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G06F30-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G06F30-15 |
| filingDate | 2020-11-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5fe4fc9191ad4b6184ac5a48d8969507 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba3a0a771903717bca73d4e97ec99836 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2efac122f327ba88dab0934d1bf7315a http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0e0b5165048ac46c2389dc4c31cf6bdf |
| publicationDate | 2021-03-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-112464359-A |
| titleOfInvention | A method for modeling and checking the flight quality of multi-rotor aircraft |
| abstract | The invention belongs to the technical field of multi-rotors, and discloses a method for modeling and checking the flight quality of a multi-rotor. The kinematic equations of three attitude angles are established. According to the dynamic equation of the multi-rotor's linear motion, the dynamic equation of rotation around the center of mass, and the kinematic equation of the three attitude angles, the flight dynamics of the nine motion state quantities of the multi-rotor are obtained. Differential equations; S3, trim the flight dynamics differential equations to obtain a balanced state; S4, perform small disturbance linearization on the flight dynamics differential equations in the balanced state, and determine the flight quality index of the multi-rotor By checking and directly simulating the multi-rotor interference problem from the basic physical theory level, the influence of transient maneuvering flight and multi-rotor interference on the rotor aerodynamic force can be considered, and the accurate multi-rotor interference flow field and aerodynamic force can be obtained. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-113094817-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-113094817-B |
| priorityDate | 2020-11-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 24.