Agile and Precise Attitude Control of Tiltrotor Aircraft in Transition Flight.
Hangxian LiuNingning WangZheshuo ZhangHui YinPublished in: IEEE Trans. Intell. Veh. (2024)
Keyphrases
- flight test
- parameter identification
- flight data
- closed loop
- nasa langley research center
- flight control
- control system
- rapid prototyping
- unmanned aerial vehicles
- air traffic control
- digital elevation models
- civil aviation
- flight path
- noise reduction
- software development
- control method
- adaptive control
- attitudes toward
- control strategy
- crew scheduling
- computer vision