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This well-known problem[^1][^2] models the ascent of a rocket through the atmosphere, and we restrict here ourselves to vertical (one dimensional) trajectories. The state variables are the altitude $r$, speed $v$ and mass $m$ of the rocket during the flight, for a total dimension of 3. The rocket is subject to gravity $g$, thrust $u$ and drag force $D$ (function of speed and altitude). The final time $T$ is free, and the objective is to reach a maximal altitude with a bounded fuel consumption.
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We thus want to solve the optimal control problem in Mayer form
[^1]: R.H. Goddard. A Method of Reaching Extreme Altitudes, volume 71(2) of Smithsonian Miscellaneous Collections. Smithsonian institution, City of Washington, 1919.
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[^2]: H. Seywald and E.M. Cliff. Goddard problem in presence of a dynamic pressure limit. Journal of Guidance, Control, and Dynamics, 16(4):776–781, 1993.
The `OptimalControl.jl` package is part of the [control-toolbox ecosystem](https://github.com/control-toolbox). It aims to provide tools to solve optimal control problems by direct and indirect methods. An optimal control problem can be described as minimising the cost functional
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```@meta
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CurrentModule = OptimalControl
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```
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The `OptimalControl.jl` package is part of the [control-toolbox ecosystem](https://github.com/control-toolbox).
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!!! note "Install"
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To install a package from the control-toolbox ecosystem,
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please visit the [installation page](https://github.com/control-toolbox#installation).
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This package aims to provide tools to solve optimal control problems by direct and indirect methods. An optimal control problem can be described as minimising the cost functional
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