Learn powerful techniques for reducing the order of differential equations, understanding first integrals, analyzing autonomous systems, and converting higher-order equations to first-order systems.
For higher-order equations, reducing the order can significantly simplify the problem. The key insight is that when certain variables are missing from the equation, we can introduce substitutions that lower the order.
Consider the -th order equation:
Case 1: If the equation has the form (missing ), substitute to get an -th order equation.
Case 2: If the equation has the form (missing ), it is called autonomous. Substitute and use .
If does not appear explicitly in , then setting and expressing higher derivatives as:
reduces the -th order equation to an -th order equation in as a function of .
Since , by the chain rule:
For the third derivative:
By induction, each can be expressed in terms of and its derivatives with respect to . ∎
Input: Higher-order ODE
Output: General solution
1. Check which variables are missing from the equation
2. If are missing:
2.1. Set
2.2. Solve the reduced equation for
2.3. Integrate times to find
3. If is missing (autonomous):
3.1. Set , express
3.2. Solve for
3.3. Integrate to find
4. return General solution with appropriate constants
Problem: Solve .
Solution:
The equation is missing . Set , so :
This is a first-order linear equation. Dividing by :
The integrating factor is . Multiplying:
Integrating to find :
A differential equation is called autonomous (or stationary) if the independent variable does not appear explicitly:
The term "autonomous" comes from the fact that the system's behavior is independent of the absolute time—only the state matters.
Problem: Solve where is mass and is a position-dependent force.
Solution:
This is autonomous (no explicit ). Set (momentum per unit mass):
The equation becomes:
Integrating both sides:
This is the energy integral: , expressing conservation of mechanical energy (kinetic + potential = constant).
The energy integral is a first integral of the equation. For conservative mechanical systems, multiplying the equation of motion by and integrating always yields the energy conservation law.
For the system where , a function is called a first integral if:
Equivalently, along solutions.
First integrals are called independent if their Jacobian with respect to the state variables is non-zero:
If where , then in a neighborhood of any regular point, the system has exactly independent first integrals.
Existence: Consider the initial value problem with . Let denote the solution. By the implicit function theorem, we can locally solve for each . These are first integrals.
Uniqueness (at most ): Taking the total derivative of any first integral:
For first integrals, the vector would be a non-trivial solution to a homogeneous system, implying the Jacobian determinant is zero—contradicting independence. ∎
If are independent first integrals of , then the general solution can be obtained by solving this system of algebraic equations for in terms of and the constants .
Problem: Find first integrals for the system , .
Solution:
This system describes rotation. Multiply the first equation by and the second by :
This gives:
For the second first integral, from we have . Substituting:
Integrating: , giving the second first integral.
Any explicit -th order ODE can be converted to a first-order system of dimension by setting:
The resulting system is:
Problem: Convert to a first-order system.
Solution:
Set and . Then:
In matrix form: where:
Converting to a first-order system is fundamental because: (1) it unifies the theory—all results for first-order systems apply, (2) numerical methods are typically designed for first-order systems, and (3) the geometric interpretation (phase space) becomes clearer.
Problem: A missile at the origin tracks a ship at moving east at speed . The missile travels at speed and always points toward the ship. Find the trajectory and interception point.
Solution:
Let be the missile position. The velocity magnitude condition:
The pointing condition (tangent toward ship at ):
Differentiating the pointing condition with respect to and using , we get:
Setting , this becomes a separable first-order equation. After solving with initial conditions :
When , the missile intercepts at , at time .