vault backup: 2025-06-12 23:41:18
Affected files: .obsidian/plugins/text-extractor/cache/19bf7bae4584f22d8d824ea9198ecda3.json .obsidian/plugins/text-extractor/cache/27f380e86244d5c5dcc79cac6cf90fde.json .obsidian/plugins/text-extractor/cache/95e163ec3e8e9050cfaaa2193f8941bd.json .obsidian/plugins/text-extractor/cache/b57b2074137d041e1b90d3b0c0e54e0e.json .obsidian/plugins/text-extractor/cache/fc6628ddefe8ab0bf9813594d700a2c0.json .obsidian/workspace.json 99 Work/0 OneSec/OneSecNotes/30 Engineering Skills/Robotics/Kalman Filter.md Attachments/Pasted image 20250612225625.png Attachments/Pasted image 20250612230042.png Attachments/Pasted image 20250612230104 1.png Attachments/Pasted image 20250612230104.png Attachments/Pasted image 20250612230414.png
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.obsidian/plugins/text-extractor/cache/19bf7bae4584f22d8d824ea9198ecda3.json
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{"path":"Attachments/Pasted image 20250612230104.png","text":"W 1 0 ° sin@ cos ¢ B(, 1:9 = c050 0 cospcosO —sin@cos0 W, ® cos@ sin¢sinf cos ¢ sin 0 W3 —— — — B 7 D 17e Û”V‘Ôîô }: j;] B/ N B/‚oß v3 ]y","libVersion":"0.3.2","langs":"deu+eng+fra"}
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{"path":"Attachments/Pasted image 20250612230042.png","text":"W 0 - sing cos® | B w, 0 =à 0 cos¢cosf —sinw@cos0 W, ® cos0 singsinf — cos®sin0 | \\w, qyYyce quves l Lz &“ 38","libVersion":"0.3.2","langs":"deu+eng+fra"}
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{"path":"Attachments/Pasted image 20250612230414.png","text":"S Roll Pitch ‘ 40 40 .…, 3 30 30 ’“ ] 3 20 I _ 20 ( _2 . Il l | …L E e — NN g < AR 1 \\ ‘ “ = Ë:;: I W Ë:;Z Ë1: -30 -30 | -40 -40 : 0 100 200 300 400 0 100 200 300 400 time (s) time (s)","libVersion":"0.3.2","langs":"deu+eng+fra"}
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"99 Work/0 OneSec/OneSecNotes/30 Engineering Skills/Robotics/Kalman Filter.md",
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@@ -65,6 +65,18 @@ $$ x_k \sim \mathcal{N}(\hat{x}_k, P_k)$$
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- Q: is the process noise: it's just there you cannot really get rid of it
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- Q: is the process noise: it's just there you cannot really get rid of it
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$$ \hat{x}^-_k = A \hat{x}_{k-1}$$
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$$ \hat{x}^-_k = A \hat{x}_{k-1}$$
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$$ P_k^- = AP_{k-1} A^T + Q$$
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$$ P_k^- = AP_{k-1} A^T + Q$$
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$$Q=\begin{pmatrix}
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\sigma_{1}^{2} & 0 & \cdots & 0\\
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0 & \sigma_{2}^{2} & \ddots & \vdots\\
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\vdots & \ddots & \ddots & 0\\
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0 & \cdots & 0 & \sigma_{n}^{2}
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\end{pmatrix}$$, where $\sigma_i^2$ is the variance of the process noise
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### Estimation Step
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### Estimation Step
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#### II. Compute Kalman Gain
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#### II. Compute Kalman Gain
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This is the dynamic update of the Kalman gain.
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This is the dynamic update of the Kalman gain.
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@@ -86,7 +98,27 @@ Note:
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- $H$: is the measurement noise: you can control it with better sensors
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- $H$: is the measurement noise: you can control it with better sensors
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### Simple Example
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## Dynamic Attitude Determination
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Sensors:
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- Gyroscope and accelerometer
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Lets integrate the gyro data to visualize what we could do to get the attitude.
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![[Pasted image 20250612230104 1.png]]
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As we can see below, there is a lot of drift meaning the numerical integration is no good.
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![[Pasted image 20250612230414.png]]
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System Model
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## Key Takeaways
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Use the Kalman filter to estimate velocity from position samples. Its much more precise than a simple derivative.
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![[Pasted image 20250612225625.png]]
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Why do IMUs have gyro and accelerometers? Because they work really well together. The gyro is fast and gives quite good data on a short time horizon, but has terrible drift. On contrary, the accelerometer is quite noisy, but gives a true value about attitude, because it can measure gravity. Thus with accelerometer measurmenets every now and then, you can fix the gyro drift and estimate it to fix it.
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Accelerometer data can give you pitch and roll. --> this is used in the kalman filter to update the estimates --> sensor fusion
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Magnetometer data can give you yaw.
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---
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---
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## Sources
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## Sources
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