| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b7c65fe2aada3b610214cbe2880d14f9 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G05D1-0623 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G05D1-08 |
| filingDate |
2006-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5d836ca0c2da308711bbb9c1ce0e896f |
| publicationDate |
2008-06-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
FR-2909462-A1 |
| titleOfInvention |
METHOD AND DEVICE FOR ACTIVE CONTROL OF THE TANGULATION OF AN AIRCRAFT. |
| abstract |
The device (1) comprises means (4) for calculating a pitch acceleration command dependent on a pitching objective and means (5) for calculating, from this pitch acceleration order, a pitch order steering of the elevators (7) of the aircraft. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9315258-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2224306-A3
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2878533-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8674851-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9058040-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9085371-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2986065-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-7853369-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3010696-A1 |
| priorityDate |
2006-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |