Boundary value problem for certain classes of nonlinear ordinary differential equations with free boundary coercivity (Q2735877)
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scientific article; zbMATH DE number 1641385
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Boundary value problem for certain classes of nonlinear ordinary differential equations with free boundary coercivity |
scientific article; zbMATH DE number 1641385 |
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25 November 2002
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boundary value problem
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nonlinear ordinary differential equations
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free boundary coercivity
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winged aircraft
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trajectory
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0.9287763
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0.9156517
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0.9142304
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0.9132143
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0.9126719
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Boundary value problem for certain classes of nonlinear ordinary differential equations with free boundary coercivity (English)
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The author considers the following problem NEWLINE\[NEWLINEm(t) \frac{dV}{dt}= k_1F(t)- f_1(V), \quad -k_2 \frac{dm}{dt}= F(t),\quad f_2(V)+ k_3F(t)= m(t) k_4,NEWLINE\]NEWLINE NEWLINE\[NEWLINE m(0)= M_0, \quad V(0)= V_0, \quad m(t_0)= m_0,NEWLINE\]NEWLINE where \(t\) varies from 0 to \(t_0\), \(f_1 (V)\) and \(f_2 (V)\) are given continuous functions on \(\mathbb{R}_+\), \(k_i\), \(M_0\), \(m_0\), and \(V_0\) are given positive constants, \(m(t)\), \(F(t)\), and \(V(t)\) are unknown functions on the interval \((0, t_0)\). The author proves that this problem is uniquely solvable. The result is used in mathematical modeling of the flight of a winged aircraft along a given trajectory.
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