Metadata-Version: 2.1
Name: matmos
Version: 0.0.0a1
Summary: Library of atmospheric models
Home-page: https://github.com/antonlopezr/matmos
Author: Antonio Lopez Rivera
Author-email: antonlopezr99@gmail.com
License: UNKNOWN
Description: # MATMOS
        
        ![alt text](tests/coverage/coverage.svg ".coverage available in tests/coverage/")
        
        MATMOS is a direct and inverse atmospheric model library. Currenty MATMOS supports 
        the International Standard Atmosphere model.
        
        MATMOS allows you to calculate the temperature, pressure and density of the atmosphere
        receiving as input a given height (direct model), or any of the other quantities 
        (indirect).
        
        As temperature is not a monotonic function of height (equal values of temperature happen 
        at different heights), its inverse cannot be determined without more information. To solve 
        this, the option to specify an altitude range where the temperature is to be found is 
        provided.
        
        [The API reference is available here]().
        
        ## Install
        
        `pip install matmos`
        
        ## Use
        
        MATMOS allows for input in the form of `float`s and well as NumPy arrays. The unit convention
        can be seen in the table below.
        
        | Magnitude | Altitude | Temperature | Pressure | Density | 
        | ---       | ---      | ---         | ---      | ---     | 
        | Unit      | km       | K           | Pa       | kg/m^3  |
         
        ### Importing a model
        
        ```
        from matmos import ISA
        ```
        
        ### Running and retrieving results
        
        The model is run by simply initializing an instance of the model with 
        height, temperature, pressure or density as inputs. 
        The results are stored as instance attributes and can be retrieved with
        the usual notation.
        
        #### Direct model
        
        Solving for a given height:
        
        ```
        m = ISA(23.5)                       # 23.5 km
        
        m.t                                 # Temperature
        m.p                                 # Pressure
        m.d                                 # Density
        ```
        
        #### Inverse model
        
        Solving for a given temperature:
        
        ```
        m = ISA(t=225, hrange=[0, 20])      # 225 K, in the range from 0 to 20 km
        
        m.h                                 # Altitude
        m.t                                 # Temperature
        m.d                                 # Density
        ```
        
        Solving for a given pressure:
        
        ```
        m = ISA(p=98000)                    # 98000 Pa
        
        m.h                                 # Altitude
        m.t                                 # Temperature
        m.d                                 # Density
        ```
        
        Solving for a given density:
        
        ```
        m = ISA(p=0.03)         # 0.03 kg/m^3
        
        m.h                     # Altitude
        m.t                     # Temperature
        m.p                     # Pressure
        ```
        
        ---
        [Back to top](#matmos)
        
Platform: UNKNOWN
Classifier: Programming Language :: Python :: 3
Classifier: License :: OSI Approved :: GNU General Public License v3 (GPLv3)
Classifier: Operating System :: OS Independent
Requires-Python: >=3.6
Description-Content-Type: text/markdown
