Development of new control algorithms for high performance autopilots
The project simulates dynamics of an aircraft subjected to an external environment that has a direct impact on the stability and behaviour of the aircraft. The Eurofighter Typhoon 2000 was chosen as the reference aircraft for the course of the project. The aircraft was subjected to open loop testing...
Saved in:
主要作者: | Raman, Akshay |
---|---|
其他作者: | Bahadir Kocer Basaran |
格式: | Final Year Project |
語言: | English |
出版: |
2015
|
主題: | |
在線閱讀: | http://hdl.handle.net/10356/65178 |
標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
機構: | Nanyang Technological University |
語言: | English |
相似書籍
-
Gain design and verification of autopilot control loops for UVAs
由: Huang, Qian.
出版: (2013) -
High level behavior for an autopilot enabled model aircraft
由: Chai, Chin Weng
出版: (2009) -
Autopilot system for micro UAV
由: Bok, Thye Boon.
出版: (2011) -
Highly-maneuverable quadcopter flight test and autopilot parameters tuning
由: Wang, Hao
出版: (2012) -
Design of flight control system and autopilot for solar UAV : part 2
由: Heng, Zeng Hui
出版: (2014)