spice | A zesty Chef server API wrapper | Frontend Framework library

I'm using Python requests and am trying to access the values that I am getting from a GET request that I have made. The output is a JSON response (I think it's called a 2D array as there are arrays within the array). I want to store these values so that I can access them in the next function.

Here is the Python:

Problem statement: When I open a file with .sp extention with vim it opens with spice syntax which the same file with .sim/.cir extension does not open with spice syntax.

My efforts: I tried by added the below line in .vimrc but it's not working.

au BufRead *.sim setfiletype spice

Details: I have the following lines in .vimrc

syntax on

filetype on

Looking for: I am looking for an option that we can add in .vimrc to enable a set of file extensions(sim/cir/sp) to open with a spice syntax.

Thanks.

So I have a function, where I want to return (resolve- upon promise completion) a set of key-value pairs, which I cannot.

I keep getting the error:

I want to print out labels of spices in SpiceContainer but I get Here is my code. How do I solve this?

I wrote 2 functions and I executed them nested. But one of my functions is not working properly. It's first line is working fine but other lines are not working. Output does not show anything. The main idea of my code is price / quality comparison. So i created 2 list and put the qualities and prices. Note: GreenGroce, Bakery etc. are the list of the prices.

Excuse me for the length of the title please but this is a pretty specific question. I'm currently simulating a launch of a rocket to mars in the 2022 launch window and I noticed that my rocket is a far distance away from Mars, even though it's traveling in the right direction. After simplifying my code to narrow down the problem, I simply plotted the orbits of the Earth and Mars (Using data from NASA's SPICE library) and propagated the position and velocity given to me by the lambert solver I implemented (Universal variables) to plot the final orbit of the rocket.

I'm only letting the Sun's gravity effect the rocket, not the Earth or Mars, to minimize my problem space. Yet even though I've simplified my problem so far, the intersection between Mars' and my rocket's orbits happens well before the time of flight has been simulated all the way, and the minimum distance between the two bodies is more than a million kilometers at all times.

That being said, something must be wrong but I cannot find the problem. I've made sure the lambert solver code I copied is correct by comparing it to Dario Izzo's method and both gave the same results. Furthermore, I've also checked that my orbit propagator works by propagating Mars' and the Earth's orbits and comparing those ellipses to the data from SPICE.

In conclusion, I assume this must be a stupid little mistake I made somewhere, but cannot find because I lack experience in this field. Thank you for any help! :)

This is the JupyterLab notebook I used:

These are the grocery store lists:

I have one requirement to iterate through list of items which has n-level of hierarchy and I would like to get bottom-up elements for the selected item ID.

For e.g. below is the raw data