3.6.10 · D1Spacecraft Structures & Systems Engineering

Foundations — Modal analysis — natural frequencies, mode shapes

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Before you can read the parent note Modal Analysis, every squiggle in its equations must mean something to you. This page builds each one from nothing — plain words first, then a picture, then why the topic cannot live without it. Read top to bottom; each block uses only things defined above it.


1. A "degree of freedom" (DOF)

The picture. Look at the two beads below. To know the whole picture at any instant you must state two numbers: how far bead 1 has moved and how far bead 2 has moved. That "how many numbers" count is the number of DOF, here .

Figure — Modal analysis — natural frequencies, mode shapes

Why the topic needs it. A real spacecraft is a smooth continuous body with infinitely many points — infinitely many DOF. We cannot compute with infinity, so Finite element analysis (FEA) chops it into a finite number of DOF. Everything downstream ( frequencies, shapes) is counted in DOF.


2. Displacement and the displacement vector

When there are several DOF we stack all their displacements into one tall column of numbers — a vector — and write it with curly braces:

Why the topic needs it. Newton's law will be written once for the whole structure using , instead of separate scribbles.


3. Velocity and acceleration — the dots

The picture. On a graph of against time, is the steepness of the curve and is how quickly that steepness itself changes — the curviness.

Why the topic needs it. Newton's law is , so acceleration must appear. Stacking all accelerations gives .


4. Stiffness and the spring force

The minus sign matters. The force always points back toward rest: pull right () and it pulls left (negative force). That restoring push is what makes things wobble instead of drifting away.

Figure — Modal analysis — natural frequencies, mode shapes

Why the topic needs it. A spacecraft's metal panels and struts behave like stiff springs. Stiffness sets how fast it wants to wobble — high stiffness pushes the natural frequency up, away from the dangerous launch frequencies described in Launch vehicle load environments.


5. Mass matrix and stiffness matrix

When springs connect several masses, each mass feels forces from its own springs and its neighbours'. Writing one Newton equation per mass and stacking them, two grids of numbers appear. Square brackets flag a matrix — a grid, rows × columns.

For the two-bead example the parent note uses:

Two words the parent leans on:

Why the topic needs it. The entire equation of motion is built from exactly these two grids. Symmetry later hands us the beautiful Orthogonality of mode shapes result for free.


6. Frequency: , , and the wobble clock

The subscript in just means natural — "the frequency the structure picks by itself when left alone," no external pushing.

Why the topic needs it. The one thing modal analysis exists to compute is this list of natural frequencies, so we may keep the forcing frequencies of launch far away from them.


7. The harmonic (sine) motion

Figure — Modal analysis — natural frequencies, mode shapes

Why the topic needs it. Assuming this exact time-shape is the trick that turns the differential equation into a plain algebra problem (the eigenvalue problem), because a sine differentiated twice is just times itself.


8. Mode shape

The picture. For the two-bead system the parent finds two shapes:

  • — both beads swing the same way (in-phase), bead 2 further.
  • — beads swing opposite ways (out-of-phase).
Figure — Modal analysis — natural frequencies, mode shapes

Why the topic needs it. The pair is mode . Knowing the shape tells engineers which part of the spacecraft moves most, so instruments needing to stay still can be placed at the calm points (nodes).


9. Transpose and the determinant

Two operations show up in the derivation; here is what each does.

Why the topic needs it. Setting the determinant to zero is the machine that spits out the natural frequencies; the transpose is the tool that later decouples the equations into simple one-DOF oscillators.


Prerequisite map

Degree of freedom

Displacement vector x

Dots for velocity and acceleration

Stiffness k and spring force

Mass matrix M and stiffness matrix K

Equation of motion

Frequency omega and f

Harmonic sine motion

Eigenvalue problem

Natural frequency omega

Mode shape phi

Transpose and determinant

Modal analysis


Equipment checklist

Cover the right side and answer out loud; reveal to check.

I can say in one sentence what a degree of freedom is
The count of independent numbers needed to fully locate the structure right now.
I know what the curly braces in signal
A column vector — a stacked list of one number per DOF.
I can read
"x-double-dot", the acceleration — displacement's rate of change taken twice.
I know why the spring force has a minus sign
It always pushes back toward rest, opposing the displacement.
I can explain an off-diagonal term in
A spring that couples two DOF, so moving one drags the other.
I know what "symmetric" means for and
Entry equals entry — the mirror across the main diagonal.
I can convert between and
, radians per second versus wobbles per second.
I know why the motion is assumed to be a sine
An undamped linear system oscillates as a pure, unending sine.
I can distinguish from
is the spatial shape of the wobble; is how fast it repeats.
I know why we set
It is the condition for a non-zero mode shape to exist.