WING TIP CONTROL EFFECTOR
WING TIP CONTROL EFFECTOR
- New search for: GUPTA RIKIN
- New search for: NAM TAEWOO
- New search for: ZHU YUFEI
- New search for: GUPTA RIKIN
- New search for: NAM TAEWOO
- New search for: ZHU YUFEI
An aircraft can include a first wing and a second wing. The first wing can extend laterally from an aircraft body to a first tip, and the second wing can extend laterally from the aircraft body to a second tip. The aircraft can include a first end effector and a second end effector, each including a fore winglet and an aft winglet. The fore and aft winglets of the first end effector can be pivotably connected to the first tip. The fore and aft winglets of the second end effector can be pivotably connected to the second tip. The fore and aft winglets of the first and second end effectors can be independently operable. The first and second end effectors can be independently operable. A processor can be operatively connected to control movement of the fore and aft winglets of the first and second end effectors.
Document information
WING TIP CONTROL EFFECTOR
2022-09-01
Patent
Electronic Resource
English
Similar titles
| British Library Conference Proceedings | 2015
Multiple control effector rate limiting
| AIAA | 1996
Multiple control effector rate limiting
| AIAA | 1995
Multiple Control Effector Rate Limiting
| Online Contents | 1996