Control system for reconfigurable rotary wing aircraft
US10025320B2 · kind B2 · utility
1Cited by
8References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Feb 15, 2012 |
| Grant date | Jul 17, 2018 |
| Priority date | — |
| Expiry date | Nov 27, 2036 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/0858
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A control system for a rotary wing aircraft having a reconfigurable element. The control system includes a model predictive control module receiving operator commands, objectives and constraints; and a dynamic inversion module receiving an output of the model predictive control module, the dynamic inversion module providing control commands to reconfigure the reconfigurable element of the rotary wing aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.