Start from the governing relation
This is the smallest equation that preserves the physics needed for the formula.
FORMULA / 019
Interactive derivation module for State-space representation.
Problem Definition
A drone attitude controller cannot be described well by one input and one output; internal states matter.
| Symbol | Quantity | Unit | Meaning |
|---|---|---|---|
| $x$ | State vector | 依系統而定 | Minimum variables needed to continue the model. |
| $A$ | System matrix | 1/s | Natural dynamics. |
| $B,C,D$ | Input/output matrices | 依系統而定 | How input enters and output is read. |
Analytical Derivation
| Item | Assumption |
|---|---|
| Assumption 1 | Linear time-invariant or locally linear behavior is assumed when using transfer functions. |
| Assumption 2 | Parameters are treated as constant over the analysis interval. |
| Assumption 3 | Numerical plots are educational approximations, not full circuit or field solvers. |
This is the smallest equation that preserves the physics needed for the formula.
The model is simplified so the dominant mechanism is visible.
The final form is the one used for design, simulation, or measurement review.
parameter $\to0$dominant term remainsThe formula reduces to its simplest physical behavior.
parameter $\to\infty$parasitics and implementation limits dominateThe closed-form equation becomes a warning rather than a full implementation model.
Parametric Verification
Use the sliders to change the physical parameters and watch the formula expose its behavior. The metric panel keeps sample count and compute latency visible so the visualization remains an engineering instrument, not only a picture.
INTERACTIVE MODULE
Engineering Application
import numpy as np
def simulate_state(A, B, x, u, dt):
return x + dt * (A @ x + B @ u)