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-3 votes
0 answers
35 views

Deriving the longitudinal equations of motion for an aircraft

I'm trying to create a state-space model for the pitch control of an aircraft as described here: https://ctms.engin.umich.edu/CTMS/index.php?example=AircraftPitch&section=SystemModeling The ...
HonHonHon's user avatar
0 votes
1 answer
26 views

High-level sun sensor modelling for satellite

I am searching for some references on how to model at high level a sensor in terms of the statistical interpretation of the errors (bias, noise, ecc). Do someone have any reference (books or papers) ...
daniele__'s user avatar
1 vote
1 answer
79 views

Optimizing Launch to LEO

I recently decided I would try to develop my own launch to LEO optimizer, as I have always been fascinated with the complexity of that problem. I have been using matlab, as I am very comfortable with ...
Frank's user avatar
  • 11
1 vote
0 answers
348 views

Designing a PID Controller for Satellite Control

As an Aerospace Engineering Student, I have been trying to make a project of a PID Controller to control the attitude response of a satellite using the parameters from a project called Kufasat. The ...
user3081005's user avatar
1 vote
1 answer
134 views

simulation of an attitude optimal Backstepping controller based quaternion for a UAV in MATLAB

I'am trying to implement this open access research article Attitude Optimal Backstepping Controller Based Quaternion for a UAV I did not find the same result in this paper Can anyone tell me where my ...
James Dilaw's user avatar
4 votes
1 answer
173 views

How to design the right input to obtain a desired output for a linear system?

If I have a state-space model, so that matrices $A$, $B$, $C$ and $D$ are known, how can I design the right input $u$, so that $y$ is a desired signal, say, a sine wave with constant amplitude? $$\...
Alessandro's user avatar