Thank you all for the 500+ likes: You can now find the model in the link in the comments
4:33. i thinks gama should be eaual to theta plus alph. am i right?
Can you send me the simulation file?
how does simulink identify or the Implementation of hardware boards types or does it only support a certain boards ?
thank bro very much but Question this model does not include internal chips types of sensors used or any schematics right its not finished project its for learning the principals only right ?
thx bro this is very interesting
Where to code this, I mean in what hardware or something. I know nothing about this topic and I want to know please help ☺
Brilliant!! Thanks for sharing
thanks for this
what kind of application would be useful for people who deal with control systems that computes in the cloud?
Can you please help what kind of functionalities would be useful?
Hi , excellent video, can you please tell me how to calculate the Y coordinates also? It will be a big help. Thanks in advance
Great video, thank you.
Can this model fit for amateur rocket model with static TVC control I'm doing a master degree "tvc control with linear and non linear commands"
How you define the blast zone?
Hi, Amazing video !!! Thanks !! Do Can you nominate content for the rocket's roll control?
Sir what type of guidance are you implementing in this? Thank you for the response :)
Love your content, dude! Super interesting stuff! PS: You're helping me a lot with my paper on quad control systems - thanks so much!
Thanks For the video, but the github is empty where is the code?
OMG! The best video ever!
Sir I am getting error at matrix multiply X_hat *K
Please please help
amazing concept...! mam
Great lecture for GNC enthusiastics, thank you sir.
Please help me in solving this problem:
The initial (3-2-1) Euler angles yaw, pitch and roll of a vehicle are (\psi, \theta, \phi)(ψ,θ,ϕ) = (40, 30, 80) degrees. Assume the body angular velocity vector of the craft is given through the BB frame components as Bωω=⎡⎣sin(0.1t)0.01cos(0.1t)⎤⎦20deg/s. Write a program to numerically integrate the yaw, pitch and roll angles over a simulation time of 1 minute. Enter the Euler angle norm \sqrt{\psi^2 + \theta^2 + \phi^2}
ψ
2
+θ
2
+ϕ
2
at the simulation time step 42s. Express angles in radians.
[Hint: if you are unsure, look at the "Optional Review: Integrating Differential Kinematic Equations" video.]
[Hint: In the integration, start with the initial angles and just integrate them without mapping them to specific quadrants
at 14:53 Nice picture of the high end HYDRA Star Tracker made by Sodern French company
The best GNC lecture I've heard.
where is Introduction to Spacecraft GN&C - Part 2 ? please guide me
Awesome lecture sir, thanks a lot
Very nicely explained sir, thanks a lot,
Great lecture, thank you so much for uploading this!
It helped me a lot in understanding the behavior of satellite ... Thank you so much for key knowledge
Awesome Lectures. Looking forward to see more from Dr. Steve Ulrich
Good information .....I look forward for your new videos
NISAR sunenge aaj sham 8 pm
It's unique method of teaching
Karman line is where air space ends and outer space starts.
100km karmon line
Sir Amazing analytical and conceptual clarity se bharpur hain aapke lectures 😊
Sir plus course kaise attend kare?
Super se upar sir ✌️
karman line
A big big thank you for giving most relevant lecture for science and technology sir🙏
Please give all the lecture for free 😔😔
Thank you sir 🙏
Karmon line😊
Studying with the best teacher ever😁
Sir, both INSAT/GSAT & GEO are providing ICT service. Then which one used for which specific service ?
Best,,sir,,बेहतरीन समझाया है
Bhut sahi revision ho rhe hai sir ❤️
jabardast sir .. first time but mja aa gya ...
Best teacher ever…. 👍
extraordinary class.... thank You sir.
Thank you sir
You are awesome sir aap real mai most different ho . Apke padane ka style sabse unique hai . Thank you sir