Ducted Fan
| Ducted Fan | |
|---|---|
| State dimension: | 1 |
| Differential states: | 6 |
| Discrete control functions: | 3 |
The Ducted Fan problem is a classical nonlinear benchmark in optimal control with multiple input and state constraints. This description is taken from [1].
It models the planar motion of a ducted fan aircraft, described by its horizontal and vertical positions , the angle with respect to the vertical, and their velocities . The inputs are the body-fixed thrust components , generated by moving flaps at the end of the duct.
The objective is to steer the fan from the origin to a horizontal position of at altitude , with zero final velocities and attitude, in a free final time , while minimising a trade-off between control effort and transition time.
Mathematical formulation
We summarize the states as .
Parameters
These fixed values are used within the model:
| Symbol | Value |
|---|---|
| 2.2 | |
| 0.05 | |
| 0.2 | |
| 4 | |
| 1 |
The weight balances control effort and transition time.
Reference Solutions
Here is one local solution to the above control problem.
- Reference solution plots
-
States and discretized control for a local optimum.
Miscellaneous and Further Reading
This formulation and a detailed description can be found in [1].
References
[1] Caillau, J.-B., Cots, O., Gergaud, J., & Martinon, P. OptimalControlProblems.jl: a collection of optimal control problems with ODE's in Julia. https://github.com/control-toolbox/OptimalControlProblems.jl/blob/main/ext/Descriptions/ducted_fan.md