Atmospheric Case 04: Dropped Sphere in Non-Rotating, Spherical Earth

Atmospheric scenario 4 tests a simple sphere with constant drag (CD = 0.1) falling from an altitude of 30,000 ft through a non-rotating spherical Earth with an initial body rotation rate of [10, 20, 30] deg/s.


Constants and Models

This scenario uses a spheroid body model with fixed inertias and aerodynamic coefficients unless otherwise specified in the scenario. The original details of the model can be found here. The 1976 STD atmosphere model defines atmospheric properties at various altitudes, specified here. The sphere's source of gravity is the inverse square gravity model, specified here. The geodesy model used for this scenario is the spheroidal non-rotating model, specified here.


Initial Conditions

Scenario Atmospheric Case 04: Dropped Sphere with Round Non-Rotating Earth
Body Atmospheric Spheroid
Geodesy Round non-rotating Earth
Atmosphere US 1976 STD; no wind
Orientation Body x-axis pointed north
Body y-axis pointed east
Body z-axis pointed down
Gravitation Inverse Square Duration 30 s
Initial states
Aerodynamic Characteristics
S (ft2)
CL
CD
CY
Cl
Cm
Cn
0.1963495
0.0
0.1
0.0
0.0
0.0
0.0
Geodetic Position
(deg, deg, ft MSL)
Latitude
Longitude
Altitude, Mean Sea Level
0
0
30,000
Velocity (NED Frame)
(ft/s)
X Velocity (North)
Y Velocity (East)
Z Velocity (Down)
0
0
0
Body Attitude (NED Frame)
(deg)
(3-2-1 Rotation)
Roll
Pitch
Yaw
0
0
0
Body Angular Rate (NED Frame) [1]
(deg/s)
Roll Rate
Pitch Rate
Yaw Rate
10
20
30

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Errata

Below is the list of erratum that are relevant to changes made on this page that no longer match the report. The full list can be found on the Home Page.

[1] Page 56, the Rate section should specify body-axis quantities relative to the local frame: Volume II Report ↩︎