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On the minimum time optimal control problem of an aircraft in its climbing phase

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Academic year: 2021

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Figure

Table 1: Constant data of a middle-haul aircraft and constant data of the atmospheric model during the climbing phase.
Figure 2: Evolution of the altitude h and of the true air speed v associated to the σ − σ s σ + structure
Figure 4: Evolution of the quantities α(·), β(·) and D 0 (x(·)) D 101 (x(·)) along the singular arc
Figure 5: Evolution of Λ(·) = det( f 0 (x(·)), f 1 (x(·)), J(·)) on [t 1 ∗ , t 2 ∗ ] where J(·) represents the Jacobi field
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