| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c1b7ebcdad16295f488a85b240b038ca |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G05D1-0202 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D45-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G05D1-02 |
| filingDate |
1972-03-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1974-01-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d42227e4f3317d3cc4f92bb54f21cd10 |
| publicationDate |
1974-01-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3788579-A |
| titleOfInvention |
Aircraft control system using inertially sensed data |
| abstract |
A system using signals available from an on-board inertial platform for controlling an aircraft through an autopilot or flight director during localizer beam capture, tracking and runway alignment modes of flight. Localizer damping is provided as a function of inertial drift angle, i. e., the angle between the heading and instantaneous ground track of the craft. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3994456-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5527003-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5505410-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4460858-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-0036771-A3
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-0036771-A2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4167735-A |
| priorityDate |
1972-03-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |