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**Describe the bug**
In the PID implementation of the multicopter attitude rate controller (https://github.com/PX4/Firmware/blob/master/src/modules/mc_att_control/RateControl/RateControl.cpp#L83), th…
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Hi,
first of all thank you for your hard work, this control toolbox on python has been very hepfull.
I've been using the LQR function in order to compute a K gain for my system but the size of i…
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Hello, I have a 2 state system I'm modeling and I want to apply a new control input at each time step, not the same input for all time steps. Can this be achieved?
Right now it looks something lik…
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I am trying to use the **LQR controller** to track state for cart_pole.
My plant was created by parsing the [cart_pole.sdf](https://github.com/RobotLocomotion/drake/blob/master/examples/multibody/c…
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# Background
What is the world model?
The robot's image or mental model of the world.
[Jay Wright Forrested](https://en.wikipedia.org/wiki/Jay_Wright_Forrester) defined a [mental model](https…
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The control log always warning `linear_quadratic_regulator.cc:56] LQR solver cannot converge to a solution, last consecutive result diff. is:0.998318`
Any suggestion for this?
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Hello,
I have linearised the model using linearizeDrone_motorcmdTotaste.slx and Simulink's Linear Analysis tool and have added a gain of K_lqr_toMotorcmd to the state_error_datin signal going into th…
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So I talked to Professor Vela and we walked through the correct way to do the path planning and motion control. Sounds like he may have actually worked with CMU 5-10 years back or something. Anyways, …
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- **Apollo version**:3.5
I have been trying to test the performance of the sample vehicle lincoln mx8 under a given complex path. After I compiled `control_component_test.cc` in `apollo/modules/con…
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Hi,
I'm encountering an error (please refer to error log at the end) when executing the command - "bash apollo.sh build". Am I missing something? appreciate your much needed help.
Thanks.
Backgro…