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Direct and indirect methods in optimal control with state constraints and the climbing trajectory of an aircraft

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Academic year: 2021

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Figure

Figure 1. A flight divided into phases
Figure 2. (a): A typical climb procedure, (1) the aircraft increases its speed at constant altitude
Table II. Description of the parameters from ISA and BADA models.
Figure 4. Evolution of the constraints and the controls along a time minimum trajectory ( α = 0.6 ) with respect to the normalized time ¯t
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