Comments (8)
giovaniceotto
commented on May 13, 2024
Methods with missing documentation are:
-
Motor
- refresh
- reshapeThrustCurve
- info - Should be simplied and allInfo should be created
- evaluateTotalImpulse
- evaluateExhaustVelocity
- evaluateMassDot
- evaluateMass
- evaluateGeometry
- evaluateInertia
- __burnRate
- importEng
- exportEng
-
Rocket
- info - Should be simplified and allInfo should be created
- refresh
- evaluateReducedMass
- evaluateTotalMass
- serMotor
- refreshStaticMargin
- addCMExcentricity
- addCPExcentricity
- addMotorExcentricity
-
Flight
- postProcess
- info
- allInfo
- animate - Should be removed, not working well
- __uDotRailOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotDrogue - Should be removed, replaced by uDotParachute
- __uDotMain - Should be removed, replaced by uDotParachute
- __uDotParachute
from rocketpy.
giovaniceotto
commented on May 13, 2024
Methods documented in branch complete_documentation as of today are:
-
Motor
- refresh - Removed - Does not make sense to have in current Motor implementation, should be replaced by more efficient version later
- reshapeThrustCurve - Documented
- evaluateTotalImpulse - Documented
- evaluateExhaustVelocity - Documented
- evaluateMassDot - Documented - Also made significantly more time efficient (~100x) by replacing setDiscrete usage by more elementary methods
- evaluateMass - Documented - Also made significantly more time efficient (~100x) by replacing integrate.odeint usage by trapezoidal rule, which gives the same result to 1e-7 accuracy
- evaluateGeometry - Documented
- evaluateInertia - Documented - Can be made much more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- __burnRate - Removed - Was rewritten inside evaluateGeometry under the name geometryDot to speed up execution and eliminate the only private method
- importEng - Documented
- exportEng - Documented
- info - Documented
- allInfo - Documented
-
Rocket
- info - Should be simplified and allInfo should be created
- refresh
- evaluateReducedMass
- evaluateTotalMass
- serMotor
- refreshStaticMargin
- addCMExcentricity
- addCPExcentricity
- addMotorExcentricity
-
Flight
- postProcess
- info
- allInfo
- animate - Should be removed, not working well
- __uDotRailOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotDrogue - Should be removed, replaced by uDotParachute
- __uDotMain - Should be removed, replaced by uDotParachute
- __uDotParachute
from rocketpy.
giovaniceotto
commented on May 13, 2024
Methods documented in branch complete_documentation as of today are:
-
Motor
- refresh - Removed - Does not make sense to have in current Motor implementation, should be replaced by more efficient version later
- reshapeThrustCurve - Documented
- evaluateTotalImpulse - Documented
- evaluateExhaustVelocity - Documented
- evaluateMassDot - Documented - Also made significantly more time efficient (~100x) by replacing setDiscrete usage by more elementary methods
- evaluateMass - Documented - Also made significantly more time efficient (~100x) by replacing integrate.odeint usage by trapezoidal rule, which gives the same result to 1e-7 accuracy
- evaluateGeometry - Documented
- evaluateInertia - Documented - Can be made much more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- __burnRate - Removed - Was rewritten inside evaluateGeometry under the name geometryDot to speed up execution and eliminate the only private method
- importEng - Documented
- exportEng - Documented
- info - Documented
- allInfo - Documented
-
Rocket
- refresh - Removed - Does not make sense to have in current Rocket implementation, should be replaced by more efficient version later
- evaluateReducedMass - Documented - Can be made 100x more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- evaluateTotalMass - Documented - Can be made 100x more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- evaluateStaticMargin - Documented - Replaced refreshStaticMargin
- setMotor - Removed - Does not make sense to have in current Rocket implementation, should be replaced by more suited version later
- addCMExcentricity - Documented
- addCPExcentricity - Documented
- addMotorExcentricity - Documented
- info - Documented
- allInfo - Documented
-
Flight
- postProcess
- info
- allInfo
- animate - Should be removed, not working well
- __uDotRailOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotOpt - Opt suffix should be removed, as this is the standard implementation
- __uDotDrogue - Should be removed, replaced by uDotParachute
- __uDotMain - Should be removed, replaced by uDotParachute
- __uDotParachute
from rocketpy.
giovaniceotto
commented on May 13, 2024
I have also added a list of attributes to the Motor class. Would be nice to do the same for the other classes.
from rocketpy.
giovaniceotto
commented on May 13, 2024
List of attributes also added to Environment class.
from rocketpy.
giovaniceotto
commented on May 13, 2024
List of attributes also added to Rocket class.
from rocketpy.
giovaniceotto
commented on May 13, 2024
Methods documented in branch complete_documentation as of today are:
-
Motor
- refresh - Removed - Does not make sense to have in current Motor implementation, should be replaced by more efficient version later
- reshapeThrustCurve - Documented
- evaluateTotalImpulse - Documented
- evaluateExhaustVelocity - Documented
- evaluateMassDot - Documented - Also made significantly more time efficient (~100x) by replacing setDiscrete usage by more elementary methods
- evaluateMass - Documented - Also made significantly more time efficient (~100x) by replacing integrate.odeint usage by trapezoidal rule, which gives the same result to 1e-7 accuracy
- evaluateGeometry - Documented
- evaluateInertia - Documented - Can be made much more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- __burnRate - Removed - Was rewritten inside evaluateGeometry under the name geometryDot to speed up execution and eliminate the only private method
- importEng - Documented
- exportEng - Documented
- info - Documented
- allInfo - Documented
-
Rocket
- refresh - Removed - Does not make sense to have in current Rocket implementation, should be replaced by more efficient version later
- evaluateReducedMass - Documented - Can be made 100x more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- evaluateTotalMass - Documented - Can be made 100x more efficient by replacing setDiscrete by more elementary methods or fixing issue #8
- evaluateStaticMargin - Documented - Replaced refreshStaticMargin
- setMotor - Removed - Does not make sense to have in current Rocket implementation, should be replaced by more suited version later
- addCMExcentricity - Documented
- addCPExcentricity - Documented
- addMotorExcentricity - Documented
- info - Documented
- allInfo - Documented
-
Flight
- postProcess - Documented
- __uDotRail - Documented - Opt suffix removed
- __uDot - Documented - Opt suffix removed
- __uDotParachute - Documented
- info - Documented
- allInfo - Documented
- animate - Quarantined as not implemented
- __uDotDrogue - Removed - Replaced by uDotParachute
- __uDotMain - Removed - Replaced by uDotParachute
from rocketpy.
giovaniceotto
commented on May 13, 2024
List of attributes also added to Flight class.
from rocketpy.
Related Issues (20)
- BUG: KeyError: 'I_11' and AttributeError: 'NoneType' object has no attribute 'reset' HOT 1
- ENH: Support for Open Meteo API
- ENH: make rocketpy classes json serializable
- ENH: adds an 3D animation of flight trajectory
- DOC: Software in a Loop (SIL) example with parachute ejection systems
- DOC: update badges on our README
- DOC: stop cloning the whole repository just for examples HOT 1
- ENH: plot inertia tensor components in a single plot
- ENH: display both power_off_drag and power_on_drag in a single plot
- ENH: adds `axial_acceleration` attribute to the Flight class HOT 2
- MNT: EmptyMotor class inherits from Motor(ABC)
- MNT: delete tools.cached_property
- DOC: convert notebooks to .rst files in the documentation
- ENH: Support for Meteomatics API
- ENH: give me a scissor or apply `Function.clip` and `Function.crop`
- BUG: Invalid Center of Pressure for Rockets with Variable Diameter
- Incorrect/incomplete docstring in environment.py HOT 4
- MNT: save ref_factor value when adding aero surfaces to a Rocket
- ENH: Allow saving plots instead of showing them HOT 3
- BLD: change setup.py to pyproject.toml HOT 1
Recommend Projects
-
React
A declarative, efficient, and flexible JavaScript library for building user interfaces.
-
Vue.js
🖖 Vue.js is a progressive, incrementally-adoptable JavaScript framework for building UI on the web.
-
Typescript
TypeScript is a superset of JavaScript that compiles to clean JavaScript output.
-
TensorFlow
An Open Source Machine Learning Framework for Everyone
-
Django
The Web framework for perfectionists with deadlines.
-
Laravel
A PHP framework for web artisans
-
D3
Bring data to life with SVG, Canvas and HTML. 📊📈🎉
-
Recommend Topics
-
javascript
JavaScript (JS) is a lightweight interpreted programming language with first-class functions.
-
web
Some thing interesting about web. New door for the world.
-
server
A server is a program made to process requests and deliver data to clients.
-
Machine learning
Machine learning is a way of modeling and interpreting data that allows a piece of software to respond intelligently.
-
Visualization
Some thing interesting about visualization, use data art
-
Game
Some thing interesting about game, make everyone happy.
Recommend Org
-
Facebook
We are working to build community through open source technology. NB: members must have two-factor auth.
-
Microsoft
Open source projects and samples from Microsoft.
-
Google
Google ❤️ Open Source for everyone.
-
Alibaba
Alibaba Open Source for everyone
-
D3
Data-Driven Documents codes.
-
Tencent
China tencent open source team.
from rocketpy.