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Hang Glider

From mintOC
Hang Glider
State dimension: 1
Differential states: 4
Discrete control functions: 2


The Hang Glider problem is a classical benchmark in optimal control. This description is taken from [1].

It consists of steering a hang glider from an initial horizontal position and altitude to a target altitude while maximising the horizontal distance travelled. The glider dynamics incorporate lift, drag, gravity, and the effect of a thermal updraft. The control variable is the lift coefficient cL, which modulates the aerodynamic lift and influences the trajectory through the thermal region.

Mathematical formulation

minux(tf)subject tox˙(t)=vx(t),y˙(t)=vy(t),vx˙(t)=L(t)w(t)+D(t)vx(t)mv(t),vy˙(t)=L(t)vx(t)D(t)wmv(t)g,x1(t)0 t[0,T],x(0)=(x0,y0,vx,0,vy,0)T,y(tf)=yfvx(tf)=vx,fvy(tf)=vy,f

with the auxiliary equations:

r(t)=(x(t)r02.5)2.Uupdraft(x)=uc(1r)er,w(t)=vy(t)Uupdraft(x),v(t)=vx(t)2+w(t)2,D(t)=12ρS(c0+c1cL(t)2)v(t)2,L(t)=12ρScL(t)v(t)2.

Parameters

These fixed values are used within the model:

Symbol Value Description
α 3 Weight on state
β 0 Weight on squared state
γ 0.5 Weight on squared control
T 10 Final time

Reference Solutions

Here is one local solution to the above control problem.

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/robbins.md