GitHub - CamiloJSO/flightdynamics-cessna310: This is a MATLAB project made for the Flight Dynamics course in the aerospace undergraduate program that allows to make an stability analysis for a Cessna 310 aircraft in approach condition.

CamiloJSO / flightdynamics-cessna310 Public

Notifications You must be signed in to change notification settings
Fork 0
Star 1

This is a MATLAB project made for the Flight Dynamics course in the aerospace undergraduate program that allows to make an stability analysis for a Cessna 310 aircraft in approach condition.

1 star 0 forks Branches Tags Activity

Star

Notifications

Branches Tags

Name		Name	Last commit message	Last commit date
Latest commit History 1 Commit
Cbsmatrix.m		Cbsmatrix.m
Cbwmatrix.m		Cbwmatrix.m
Cessna310_approach_aircraft.m		Cessna310_approach_aircraft.m
DCM.m		DCM.m
H.m		H.m
Hinv.asv		Hinv.asv
Hinv.m		Hinv.m
Navion_aircraft.m		Navion_aircraft.m
aerodynamics.m		aerodynamics.m
analyzeAircraftDynamicModes.m		analyzeAircraftDynamicModes.m
atmosphere.m		atmosphere.m
f.m		f.m
faircraft.m		faircraft.m
ftrimPullup.m		ftrimPullup.m
ftrimRect.asv		ftrimRect.asv
ftrimRect.m		ftrimRect.m
ftrimRoll.asv		ftrimRoll.asv
ftrimRoll.m		ftrimRoll.m
ftrimTurn.m		ftrimTurn.m
homework2.m		homework2.m
linearizeAircraftModel.m		linearizeAircraftModel.m
loadFactor.m		loadFactor.m
plotAircraftSimulationResults.m		plotAircraftSimulationResults.m
propulsion.m		propulsion.m
simulateAircraft.m		simulateAircraft.m
tesTrimConditionsRect.asv		tesTrimConditionsRect.asv
testLinearizeAircraftModel.m		testLinearizeAircraftModel.m
testTrimConditionsPullup.m		testTrimConditionsPullup.m
testTrimConditionsRect.m		testTrimConditionsRect.m
testTrimConditionsRoll.m		testTrimConditionsRoll.m
testTrimConditionsTurn.asv		testTrimConditionsTurn.asv
testTrimConditionsTurn.m		testTrimConditionsTurn.m
trimConditionsPullup.m		trimConditionsPullup.m
trimConditionsRect.m		trimConditionsRect.m
trimConditionsRoll.m		trimConditionsRoll.m
trimConditionsTurn.m		trimConditionsTurn.m

About

This is a MATLAB project made for the Flight Dynamics course in the aerospace undergraduate program that allows to make an stability analysis for a Cessna 310 aircraft in approach condition.

matlab flight-dynamics cessna310

Activity

1 star

1 watching

0 forks

Report repository