The stabilization of the equilibrium of conservative systems using gyroscopic forces (Q2761256)
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scientific article; zbMATH DE number 1683313
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | The stabilization of the equilibrium of conservative systems using gyroscopic forces |
scientific article; zbMATH DE number 1683313 |
Statements
18 December 2001
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conservative holonomic system
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instability conditions
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equilibrium
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gyroscopic forces
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stability of artificial satellite
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0.95879984
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0.9556774
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0.94142765
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The stabilization of the equilibrium of conservative systems using gyroscopic forces (English)
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The author considers a conservative holonomic system with \(n\) degrees of freedom \(\frac{d}{dt}\frac{\partial L}{\partial\dot q}- \frac{\partial L}{\partial q} = 0\), where \(L(q,\dot q) = L_2(q,\dot q) + L_1(q,\dot q) + L_0(q) = \frac 12 \dot q^TA(q)\dot q+f(q)^T\dot q+L_0(q)\). It is assumed that \(L(q,\dot q)\in C^2(D_q\times \mathbb{R}^n)\); the quadratic form \(L_2(0,\dot q)\) is positive definite, the point \(q = \dot q = 0\) corresponds to the equilibrium state of the system, and \(f(0) = L_0(0) = 0\). Under some additional assumptions the author derives instability conditions for the equilibrium of the system under gyroscopic forces.
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