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13 changes: 7 additions & 6 deletions docs/Project.toml
Original file line number Diff line number Diff line change
Expand Up @@ -9,10 +9,11 @@ OrdinaryDiffEq = "1dea7af3-3e70-54e6-95c3-0bf5283fa5ed"
Plots = "91a5bcdd-55d7-5caf-9e0b-520d859cae80"

[compat]
ForwardDiff = "0.10.36"
MINPACK = "1.2.0"
NLPModelsIpopt = "0.10.2"
OptimalControl = "0.9.4"
OrdinaryDiffEq = "6.85.0"
Plots = "1.40.5"
Documenter = "1.6"
ForwardDiff = "0.10"
MINPACK = "1.2"
NLPModelsIpopt = "0.10"
OptimalControl = "0.11"
OrdinaryDiffEq = "6.88"
Plots = "1.40"
julia = "1.10"
10 changes: 10 additions & 0 deletions docs/src/index.md
Original file line number Diff line number Diff line change
Expand Up @@ -231,6 +231,16 @@ plt1 = plot3d(1; xlim = (-60, 60), ylim = (-60, 60), zlim = (-5, 5), title = "Or
end every N ÷ min(N, 100)
```

## Dependencies

All the numerical simulations to generate this documentation are performed with
the following packages.

```@example
using Pkg
Pkg.status()
```

## References

[^1]: Bonnard, B.; Caillau, J.-B.; Trélat, E. Geometric optimal control of elliptic Keplerian orbits. *Discrete Contin. Dyn. Syst. Ser. B* **5** (2005), no. 4, 929-956.
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