diff --git a/chapter-1.html b/chapter-1.html index 0236701..02f0402 100644 --- a/chapter-1.html +++ b/chapter-1.html @@ -278,179 +278,185 @@
- + 1.2 Hamilton’s variational principle
- + 1.3 First steps with conserved quantities
- + 1.4 Euler-Lagrange equations on smooth manifolds
- + 2.2 The spherical pendulum
- + 2.3 Intermezzo: small oscillations
- + 2.4 Motion in a central potential
- + 2.5 D’Alembert principle and systems with constraints
- + 3.1 The Legendre Transform in the euclidean plane
- + 3.2 Intermezzo: cotangent bundle and differential forms
- + 3.3 The Legendre Transform
- + 3.4 Poisson brackets and first integrals of motion
- + 3.5 Variational principles of hamiltonian mechanics
- + 3.6 Canonical transformations
- + 3.7 The symplectic structure on the cotangent bundle
- + 4.1 Lagrangian submanifolds
- + 4.2 Canonical transformations revisited
- + 4.3 Hamilton-Jacobi equations
- + 4.4 The Liouville-Arnold theorem
- + 5 Hamiltonian perturbation theory
- + 5.1 Small oscillations revisited
- + 5.3 A brief look at KAM theory
++ +Index +
+ + @@ -659,9 +665,10 @@-In the elementary formulation we will focus on, our primary interest is in describing the equations of motion for an idealized point particle. This is a point–like object obtained by ignoring the dimensions of the physical object. Note that in -many cases this is a reasonable first approximation. For example, when describing planetary motion around the sun, we can consider the planet and the sun as two point particles without significantly affecting the qualitative properties of the system. -After all the sun is about 150 million kilometers away from the Earth, compared to which their sizes are negligible. The diameter of the sun is just 0.9% of this distance and the diameter of the Earth a mere 0,008%. +In the elementary formulation we will focus on, our primary interest is in describing the equations of motion for an idealized point particle. This is a point–like object obtained by ignoring the dimensions of the +physical object. Note that in many cases this is a reasonable first approximation. For example, when describing planetary motion around the sun, we can consider the planet and the sun as two point particles without significantly affecting the +qualitative properties of the system. After all the sun is about 150 million kilometers away from the Earth, compared to which their sizes are negligible. The diameter of the sun is just 0.9% of this distance and the diameter of the Earth a mere +0,008%. See Figure 1.1.
@@ -693,7 +702,7 @@-A point particle is first of all a point, a dimensionless mathematical object in space: its position in space is described by the position vector \(\vb *{x} = (x, y ,z)\). Keep in mind that +A point particle is first of all a point, a dimensionless mathematical object in space: its position in space is described by the position vector \(\vb *{x} = (x, y ,z)\). Keep in mind that
\(\seteqnumber{0}{}{0}\) @@ -718,7 +727,7 @@-The velocity of the point particle is given by the rate of change of the position vector, i.e., its derivative with respect to time1 +The velocity of the point particle is given by the rate of change of the position vector, i.e., its derivative with respect to time1
\(\seteqnumber{0}{}{1}\) @@ -739,7 +748,7 @@-We call acceleration, the rate of change of the velocity, i.e., the second derivative +We call acceleration, the rate of change of the velocity, i.e., the second derivative
\(\seteqnumber{0}{}{2}\) @@ -762,13 +771,13 @@For us, the main distinction between a mathematical point and a point particle, is that the latter usually carries a mass \(m\). This is a scalar quantity that, as we will see, measures its resistance to changes in its state of motion, also -known as inertia. +known as inertia.
-1 Notation: the symbol \(a := b\) means that \(a\) is defined by the expression \(b\), similarly \(b =: a\) is the same statement but read from right to left. +1 Notation: the symbol \(a := b\) means that \(a\) is defined by the expression \(b\). Similarly \(b =: a\) is the same statement but read from right to left.
@@ -781,14 +790,27 @@+Newton’s second law of motion +
+-The mechanics of the particle is encoded by Newton’s second law of motion. That is, there exist frames of reference (i.e systems of coordinates) in which the motion of the particle is described by a differential equation involving -the forces \(\vb *{F}\) acting on the point particle, its mass \(m\) and its acceleration as follows2 +There exist frames of reference, that is, systems of coordinates, in which the motion of the particle is described by a differential equation involving the forces \(\vb *{F}\) acting on the point particle, its mass +\(m\) and its acceleration as follows
\(\seteqnumber{0}{}{3}\) @@ -808,43 +830,18 @@-2 This is not completely true, Newton was already talking about momentum, which makes a deep difference but would set us off-course right now. -
- --Let’s leave it here for now, we will come back to it later on. +Note that the law as described above is not completely true: Newton was already talking about momentum, which makes a deep difference, but would set us off-course right now.
-In general we will consider systems of \(N\) point particles. These will be described by a set of \(N\) position vectors \(\vb *{x}_k = (x_k, y_k ,z_k)\) with masses \(m_k\), \(k = 1, \ldots , N\). For convenience we will denote3 -\(\vb *{x} = (\vb *{x}_1, \ldots , \vb *{x}_N)\in \mathbb {R}^{3N}\), and \(\vb *{m} = (m_1, \ldots , m_N)\in \mathbb {R}^N\). We call \(\vb *{x}(t)\) the configuration of the system at time \(t\) in the -configuration space \(\mathbb {R}^{3N}\). +Before moving on, let’s anticipate three examples that will come back over and over in the course of this book. Here we will just sketch them, but we will come back to them in more detail later.
--3 Here we are identifying \(\mathbb {R}^{3\times N}\), the space of \(3\times N\) matrices, and \(\mathbb {R}^{3N}\), the space of \(3N\) vectors. Namely, \(\vb *{x} = (\vb *{x}_1, \ldots , \vb *{x}_N) = (x_1, y_1, -z_1, x_2, y_2, z_2, \ldots , x_N, y_N, z_N)\) is used interchangeably as the vector of positions of the points in three-space or as the vector including all the positions of the \(N\) bodies together. -
- - -- -Example 1.1. For example a system of two rigid pendulums in space -constrained to oscillate on a vertical plane, is described by two position vectors, so \(\vb *{x} = (\vb *{x}_1, \vb *{x}_2)\in \mathbb {R}^{6}\). However, to describe their configuration we only need two angular variables, one for each of the -pendulums. So, for all practical purposes, the system could be completely described4 by \(q = (q^1, q^2) \in \mathbb {S}^1\times \mathbb {S}^1 \simeq \mathbb {T}^2\). See Figure 1.2. -
- --4 Here there is an hidden statement: \(\mathbb {S}^1\times \mathbb {S}^1 \simeq \mathbb {T}^2\). This should be read as: the 2-torus, the surface of a doughnut, is diffemorphic to the product of two circles. Here, -diffeomorphic is a concept from the theory of smooth manifolds, and stands for the existence a smooth bijection between the two constructions. Note that \(\simeq \) usually denotes some kind of equivalence, but which specific kind is -context-dependent and not often well explicited. + +Example 1.1 (Horizontal spring and pendulum). Consider an ideal spring, that is, an idealized system consisting of a point particle of mass \(m\) attached to a spring with stiffness \(k\), sliding on a frictionless surface. +Assume that the motion is one-dimensional, along the axis of the spring, and let \(x\) denote the displacement of the system from its equilibrium position, i.e., the position in which the spring is completely at rest: not compressed nor extended. It is +convenient to assume that the sliding happens on a flat surface. This allows us to exclude gravitational forces from the picture, making this example as simple as it could be.
- - --We say that a system of \(N\) particles has \(n\) degrees of freedom if we need \(n\) independent parameters to uniquely specify the system configuration5. We call generalized -coordinates any set of \(n\) parameters \(q = (q^1, \ldots , q^n)\) that uniquely determine the configuration of a system with \(n\) degrees of freedom, and generalized velocities their time derivatives \(\dot q = (\dot q^1, -\ldots , \dot q^n)\). The state of the system is then characterized by the set of (generalized) coordinates and velocities \((q, \dot q) = \left (q^1, \ldots , q^n,\dot q^1, \ldots , \dot q^n\right )\). -
- --If you recall differential geometry, you may (correctly) guess that the generalized coordinates will be points on some differentiable manifold \(q\in M\), their evolution will be described by a curve \(q: \mathbb {R} \to M\) parametrized by time and -the state of the system will be a point in the tangent bundle \((q, \dot q)\in TM\), i.e., \(\dot q \in T_q M\) (see also section 1.4). -
- --We have now all the elements to translate the Newtonian principle of determinacy in mathematical terms. In 1814, Laplace [Lap51] wrote -
-- -- --We may regard the present state of the universe as the effect of its past and the cause of its future. An intellect which at a certain moment would know all forces that set nature in motion, and all positions of all items of which nature is composed, if -this intellect were also vast enough to submit these data to analysis, it would embrace in a single formula the movements of the greatest bodies of the universe and those of the tiniest atom; for such an intellect nothing would be uncertain and the -future just like the past would be present before its eyes. -
-
-In other words, this principle states that the initial state \(\left (q(t_0), \dot q(t_0)\right )\) uniquely determines its evolution \(\left (q(t),\dot q(t)\right )\) for \(t > t_0\). The Picard-Lindelöf theorem6 implies that the Newtonian principle of determinacy is locally satisfied by the equations of motion of the mechanical system, i.e., second order differential equations derived from Newton’s law. -
--5 As Example 1.1 shows, the \(n\) degrees of freedom do not have to be the cartesian coordinates of the point particles. -
- --6 Also known as “Existence and uniqueness of solutions of initial value problems”, [Kna18, Theorem 3.17]. -
- - --Before taking a little detour into Lagrangian mechanics, let’s anticipate some of the upcoming concepts in a few simple cases. -
-- -Example 1.2 (Horizontal spring and pendulum). Consider an idealized system consisting of a point particle of mass \(m\) attached to a spring with stiffness \(k\), sliding on a frictionless surface. Assume that the motion is one-dimensional along the axis of the spring and let -\(x\) denote the displacement of the system from its equilibrium position, i.e., the position in which the spring is completely at rest: not compressed nor extended. We consider this system to exclude gravitational forces from the picture. -
- --Hooke’s law states that the restoring force \(F\) exerted by the spring on whatever is pulling its free end scales linearly with respect to the distance it’s been pulled: i.e., \(F(x) = - k x\), see Figure 1.3 left. According to (1.4), then, the motion of the point particle is given by +Hooke’s law states that the restoring force \(F\) exerted by an ideal spring is directly proportional to its displacement \(x\) from equilibrium. The law is expressed mathematically as \(F(x) = -kx\), where +\(k\) is the spring constant, a measure of the spring’s stiffness. The negative sign indicates that the force acts in the opposite direction of the displacement, always seeking to restore the spring to its equilibrium position. +See Figure 1.2, left panel. According to (1.4), then, the motion of the point particle is given by
\(\seteqnumber{0}{}{4}\) @@ -981,9 +898,9 @@-with the unknowns \(R\) and \(\phi \) uniquely prescribed by the initial conditions +with the unknowns \(R\in \mathbb {R}\) and \(\phi \in [0,2\pi )\) uniquely prescribed by the initial conditions
\(\seteqnumber{0}{}{6}\) @@ -1031,7 +948,7 @@-Clearly, once we know the initial conditions, the full evolution of the solution \(x(t)\) is known, in agreement with Newton’s principle of determinacy. +Once we know the initial conditions, the full evolution of the solution \(x(t)\) is known.
- - --Consider, now, a point particle of mass \(m\) attached to a pivot on the ceiling via a rigid rod of length \(l\). Assume the motion is frictionless and happening only in the vertical direction. Let \(x\) denote the angle of displacement of the system -from its equilibrium position, i.e., the lowest point on the arc of motion. Take the angle at equilibrium to be zero, with positive sign on the right hand side of the vertical, and negative on the left. +Consider, now, an ideal pendulum . That is, a point particle of mass \(m\) attached to a pivot on the ceiling via a rigid rod of length \(l\). Assume the motion is frictionless and happening only in a vertical plane. Let +\(x\) denote the angle of displacement of the system from its equilibrium position on this plane, i.e., the lowest point on the arc of motion. Without loss of generality, we can assume the angle at equilibrium to be zero, with positive sign on the right +hand side of the vertical, and negative on the left. See Figure 1.2, right panel.
@@ -1093,9 +982,9 @@
-Although it is possible to solve the equation of motion of the pendulum by means of elliptic integrals, this is rather cumbersome. Under certain conditions, when \(\sin x \approx x\), we can actually avoid doing this and instead we use the -equation of the spring as a model for the pendulum oscillation via the so-called called small oscillations approximation. We will come back to this later on. +Although it is possible to solve the equation of motion of the pendulum explicitl yby means of elliptic integrals [Eur24], this is rather cumbersome. In some cases, when \(\sin x \approx x\), we can simplify our life and, instead, use the equation of the spring as a model for the pendulum oscillation via +the so-called small oscillations approximation. We will come back to this later on.
- -Example 1.3 (Idealized motion of the Earth around the Sun). - Let us approximate the Sun with a point particle of mass \(M\) positioned at the origin \(\vb *{0}\in \mathbb {R}^3\) of the Euclidean space. In this solar system, with the Sun fixed at the origin, we will -describe the Earth by a point particle of mass \(m\) whose position (and motion) is described by a vector \(\vb *{x}\in \mathbb {R}^3\). + +Example 1.2 (Idealized motion of the Earth around the Sun). + Let us approximate the Sun with a point particle of mass \(M\) positioned at the origin \(\vb *{0}\in \mathbb {R}^3\) of the Euclidean space. In this model of the solar system, with the Sun fixed at the origin, +we will describe the Earth by a point particle of mass \(m\) whose position (and motion) is described by a vector \(\vb *{x}\in \mathbb {R}^3\).
-Due to our choice of coordinates, the gravitational attraction of the Sun acts in direction \(-\vb *{x}(t)\). Newton’s law of universal gravitation says that such a force is proportional to +Due to our choice of coordinates, the gravitational attraction of the Sun acts in the direction of \(-\vb *{x}(t)\). Newton’s law of universal gravitation says that such a force is proportional to
\(\seteqnumber{0}{}{8}\) @@ -1146,9 +1036,9 @@-where \(G \sim 6.674 \cdot 10^{-11} \frac {m^3}{s^2\,kg}\) is called the gravitational constant. Once we collect all the elements into Newton’s second law (1.4), we obtain the equation of motion +where \(G \sim 6.674 \cdot 10^{-11} \frac {m^3}{s^2\,kg}\) is called the gravitational constant. Newton’s second law (1.4), +then, leads to the equation of motion
\(\seteqnumber{0}{}{9}\) @@ -1172,8 +1062,8 @@This is an autonomous second order ordinary differential equation on the configuration space \(\mathbb {R}^3\setminus \big \{\vb *{0}\big \}\). Providing the initial conditions \(\vb *{x}(0)=\vb *{x}_0\) and \(\dot {\vb *{x}}(0)=\vb -*{v}_0\), we can try to explicitly solve (1.10), however in this case we could already get a lot of insight by taking a slightly different point of view. +*{v}_0\), we can try to solve (1.10), and you are welcome to try. As it is often the case, though, things can become easier by taking a step back and looking at the +problem differently.
-Behind differential equations in classical mechanics lies a surprisingly rich geometrical structure, in which conserved quantities play a special role. These can help to obtain extensive information on the solution of classical equations of motion without -the need to explicitly solve the equations (which would be, in general, impossible). +Behind differential equations in classical mechanics lies a surprisingly rich geometrical structure, in which symmetries and conserved quantities play a special role. These can help to obtain extensive information on the solution of classical equations of +motion without the need to explicitly solve the equations (which, in general, is impossible). Let’s have an initial brief look at this in the context of the Kepler problem.
-On the tangent bundle \((\mathbb {R}^3\setminus \big \{\vb *{0}\big \})\times \mathbb {R}^3\), let us define the total energy +Consider the space \(\big (\mathbb {R}^3\setminus \big \{\vb *{0}\big \}\big )\times \mathbb {R}^3\), and define there, for the moment without further justification or explanation, the total energy function
\(\seteqnumber{0}{}{10}\) @@ -1208,7 +1099,7 @@-Along the solutions of (1.10), let us define \(E(t):=E(\vb *{x}(t),\dot {\vb *{x}}(t))\) and, similarly, \(L(t)\) and \(A(t)\). Then, there exist solutions such that -\(L(t) = L(0) \neq 0\) for all times, and also \(E(t) = E(0)\) and \(A(t) = A(0)\). Furthermore, a solution that lives on the “submanifold” defined by +Along the solutions \(\vb *{x}(t)\) of (1.10), let us define \(E(t) := E(\vb *{x}(t),\dot {\vb *{x}}(t))\) and, similarly, \(L(t)\) and \(A(t)\).
++In due time we will show that, \(L(t) = L(0) \neq 0\) for all times, and also \(E(t) = E(0)\) and \(A(t) = A(0)\) are constant for all times. Furthermore, any solution that lives on the subspace defined by +
\(\seteqnumber{0}{}{13}\) + + + (x, v) ∈ R3 \ 0 × R3 | E(x, v) = E(x0 , v 0 ), L(x, v) = L(x0 , v 0 ), A(x, v) = A(x0 , v 0 ) , (1.14) + --\begin{equation} -\begin{aligned} \big \{ & (\vb *{x}, \vb *{v})\in (\mathbb {R}^3\setminus \big \{\vb *{0}\big \})\times \mathbb {R}^3 \;\mid \\ & \; E(\vb *{x},\vb *{v}) = E(\vb *{x}_0, \vb *{v}_0),\; L(\vb *{x},\vb *{v}) -= L(\vb *{x}_0, \vb *{v}_0),\; A(\vb *{x},\vb *{v}) = A(\vb *{x}_0, \vb *{v}_0) \big \}, \end {aligned} -\end{equation} + +--> -
+ + +\begin{align} +\big \{ (\vb *{x}, \vb *{v})\in \big (\mathbb {R}^3\setminus \big \{\vb *{0}\big \}\big )\times \mathbb {R}^3 \;\mid \; E(\vb *{x},\vb *{v}) = E(\vb *{x}_0, \vb *{v}_0),\; L(\vb *{x},\vb *{v}) = L(\vb *{x}_0, \vb +*{v}_0),\; A(\vb *{x},\vb *{v}) = A(\vb *{x}_0, \vb *{v}_0) \big \}, +\end{align} must be a conic of the following type
@@ -1311,7 +1205,7 @@This is an example of a central force field, and is one of the most prominent and most important examples in this course. The impatient reader can find in [Kna18, Ch. 1] a nice and -compact derivation of Kepler’s laws and the invariants above from (1.10) and its solutions. +compact derivation of Kepler’s laws and the invariants above from (1.10).
+It is a bit limiting to consider only systems with one particle and, indeed, many interesting problems in classical mechanics involve systems on interacting particles. +
-In order to leave more space to discuss Hamiltonian systems and their geometry, we will be brief7 in our account of Lagrangian mechanics and calculus of variations. For a more detailed account refer to [Arn89, Part II]. This, however, should not confuse you: Lagrangian mechanics plays a role as large as Hamiltonian mechanics in the development of classical mechanics. +In general a system of \(N\) point particles will be described by a set of \(N\) position vectors \(\vb *{x}_k = (x_k, y_k ,z_k)\) with masses \(m_k\), \(k = 1, \ldots , N\). For convenience we will denote \(\vb *{x} += (\vb *{x}_1, \ldots , \vb *{x}_N)\in \mathbb {R}^{3N}\), and \(\vb *{m} = (m_1, \ldots , m_N)\in \mathbb {R}^N\). We call \(\vb *{x}(t)\) the configuration of the system at time \(t\) in the +configuration space \(\mathbb {R}^{3N}\).
-In fact, one should not be surprised if there are many sources claiming that the most general formulation of the equations of motion in classical mechanics comes from the principle of least action or Hamilton’s variational principle. +Note that we are identifying \(\mathbb {R}^{3\times N}\), the space of \(3\times N\) matrices, and \(\mathbb {R}^{3N}\), the space of \(3N\) vectors. Namely, \(\vb *{x} = (\vb *{x}_1, \ldots , \vb *{x}_N) = (x_1, y_1, z_1, x_2, +y_2, z_2, \ldots , x_N, y_N, z_N)\) is used interchangeably as the vector of positions of the points in three-space or as the vector including all the positions of the \(N\) bodies together.
+-According to this principle, stated in 1834, the equations of motion of a mechanical system are characterized by a function \(L \equiv L(q, \dot q, t) : \mathbb {R}^n \times \mathbb {R}^n \times \mathbb {R} \to \mathbb {R}\), called -the lagrangian (function) of the system. + +Example 1.3. A system of two ideal pendulums is described by two +position vectors, so \(\vb *{x} = (\vb *{x}_1, \vb *{x}_2)\in \mathbb {R}^{6}\). Notice, however, that to describe their configuration we only need two angular variables, one for each of the pendulums. So, for all practical purposes, +the system could be completely described by \(q = (q^1, q^2) \in \mathbb {S}^1\times \mathbb {S}^1 \simeq \mathbb {T}^2\). See Figure 1.3. +
+ +