Abstract
The Delft University laboratory aircraft Cessna Citation II has the capability to implement and test new auto pilot control laws. The aircraft is equipped as a Fly-By-Wire testbed, that enables the user to control the aircraft through an experimental computer and directly have control over the control surfaces. An extra control stick is mounted on the righthand side in the cockpit from where the aircraft can be controlled in a closed loop. The gains can be adjusted in-flight. An experimental display in the cockpit showed the setpoints for the rate and direct control in pitch and roll.
The control laws that were tested are developed by the department of aircraft systems dynamics of the German Aerospace Center together with Delft University of Technology. The control laws are based on Incremental Nonlinear Dynamic Inversion (INDI). INDI uses synchronized measurements or estimations of (angular) accelerations and control surface deflections. This way it is not dependent on an airplane model, but it is able to automatically adapt flight control laws to changing dynamic behavior of the aircraft, even in case of major system failures or damage to the airframe. The INDI controller directly controls the current to the control surface actuators.
This paper treats the execution of the test flights.
The control laws that were tested are developed by the department of aircraft systems dynamics of the German Aerospace Center together with Delft University of Technology. The control laws are based on Incremental Nonlinear Dynamic Inversion (INDI). INDI uses synchronized measurements or estimations of (angular) accelerations and control surface deflections. This way it is not dependent on an airplane model, but it is able to automatically adapt flight control laws to changing dynamic behavior of the aircraft, even in case of major system failures or damage to the airframe. The INDI controller directly controls the current to the control surface actuators.
This paper treats the execution of the test flights.
| Original language | English |
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| Title of host publication | Society of Flight Test Engineers - European Chapter Symposium |
| Place of Publication | Delft, Netherlands |
| Number of pages | 10 |
| Publication status | Published - 30 May 2018 |
| Event | 29th Society of Flight Test Engineers European Chapter symposium: The Fewer Aircraft To Flight Test, The More Reason To Share Experience - Faculty of Aerospace Engineering of the Delft University of Technology , Delft, Netherlands Duration: 29 May 2018 → 31 May 2018 Conference number: 29 http://Faculty of Aerospace Engineering of the Delft University of Technology |
Conference
| Conference | 29th Society of Flight Test Engineers European Chapter symposium |
|---|---|
| Abbreviated title | SFTE EC Symposium 2018 |
| Country/Territory | Netherlands |
| City | Delft |
| Period | 29/05/18 → 31/05/18 |
| Internet address |