http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-115167492-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_aa290cfbc4cd90be40bdc3dfa6829f54 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G05D1-0808 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G05D1-08 |
| filingDate | 2022-07-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_20f6ea673067329c2d0c116588f5a065 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e43383a03a9424247f9bdb44608e181e http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ac61c6b395a8b73ce4cb7af64dce9fee |
| publicationDate | 2022-10-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-115167492-A |
| titleOfInvention | A Li Yave Adaptive Attitude Control Method for UAV Obstacles |
| abstract | The invention relates to an adaptive attitude control method of UAV obstacle Li Yave. It measures the pitch attitude angle of the UAV by installing the attitude gyroscope, and installs the rate gyroscope to measure the pitch angle rate signal of the UAV; sets the desired pitch angle signal and compares it with the pitch attitude angle signal to obtain the attitude angle error signal, and set it up. The attitude tracking control method is used to increase the stability of the UAV by determining the attitude angle obstacle point, the angular rate obstacle point and the acceleration obstacle point. By designing the obstacle Li Yave adaptive control method, the UAV is close to the above obstacle points in the flight state. The method of generating a larger control torque at the same time, so as to converge to the desired state more quickly, finally realizes the stable attitude flight of the UAV, and also has the advantages of better stability guarantee. |
| priorityDate | 2022-07-23-04:00^^<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/SID419559589 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID119434 |
Total number of triples: 15.