44 Government Documents Referencing a Flat and/or Non-Rotating Earth

US STANDARD ATMOSPHERE 1962.pdf (33.7 MB)

User Manual for the Microsoft Window Edition of the Scanning Fast-Field Program.pdf (4.4 MB)

TTP for the Field Artillery Cannon Gunnery.pdf (7.4 MB)

Tian et al - Design and Implementation of Flight Visual Simulat.pdf (2.4 MB)

THE PRODUCTION OF FIRING TABLES FOR CANNON ARTILLE.pdf (4.1 MB)

The Development and Validation of a Piloted Simulation of a Helicopter and External Sling Load.pdf (39.7 MB)

Telemetry Standards - 106-17.pdf (15.8 MB)

Tactics Techniques and Procedures for the Field Artillery Manual Cannon Gunnery.pdf (27.4 MB)

Sturgeon and Phillips - A Mathematical Model of the CH-53 Helicopter.pdf (1.5 MB)

Singular-Arc Time-Optimal Trajectory of Aircraft in Two-Dimensional Wind Field.pdf (1.1 MB)

THE PRODUCTION OF FIRING TABLES FOR CANNON ARTILLE.pdf (4.1 MB)

Propagation of Electromagnetic Fields Over Flat Earth.pdf (355.1 KB)

Preisser - AND SIDESLIP FROM RADAR DATA AND A ROLL-STABILIZED.pdf (1.3 MB)

Piester et al - STUDIES ON INSTABILITIES IN LONG-BASELINE TWO-WAY .pdf (359.0 KB)

Path-Loss Measurements in a Forested Environment at VHF.pdf (3.3 MB)

Nyborg and Mintzer - 1955 - REVIEW OF SOUND PROPAGATION IN THE LOWER ATMOSPHER.pdf (13.5 MB)

Norlin - 1995 - Flight simulation software at NASA Dryden Flight R.pdf (3.8 MB)

Moes and Iliff - 2002 - Stability and Control Estimation Flight Test Resul.pdf (1.6 MB)

Modeling of Atmospheric Effects.pdf (642.2 KB)

Mcnally and Bach Jr - 1988 - Flight testing a VSTOL aircraft to identify a ful.pdf (692.6 KB)

Ma and Arce - Beacon Position and Attitude Navigation Aided by a.pdf (889.1 KB)

Lineberger - ATMOSPHERIC OSCILLATIONS.pdf (1.2 MB)

James - CALCULATION O F WIND COMPENSATION FOR LAUNCHING OF.pdf (1.9 MB)

Investigation of Aircraft Landing in Variable Wind Effects.pdf (3.7 MB)

Goldman - Computationally Efficient Algorithms for Estimatin.pdf (2.6 MB)

Field Artillery Manual Cannon Gunnery.pdf (39.0 MB)

Ferguson - A Mathematical Model for Real Time Flight Simulati.pdf (27.7 MB)

Feeley - Approximate Optimal Guidance for the Advanced Laun.pdf (3.9 MB)

Elliott and ReseurchCenter - A METHOD FOR REDUCING THE SENSITIVITY OF OPTIMAL N.pdf (1.3 MB)

Duke et al. - User’s Manual for LINEAR , a FORTRAN Program to D.pdf (3.8 MB)

Duke et al. - Derivation and Definition of a Linear Aircraft Mod.pdf (3.2 MB)

Dissertations Defended in the Scientific Council of the Institute of Physics of the Earth.pdf (4.0 MB)

Derivation of a Point-Mass Aircraft Model used for.pdf (669.7 KB)

Der et al. - 2002 - Automatic Target Acquisition of the DEMO III Progr.pdf (1004.1 KB)

Der et al. - 2001 - Scale-Insensitive Detection Algorithm for FLIR Ima.pdf (2.1 MB)

Cooper - 2011 - Trajectory Prediction of Spin-Stabilized Projectil.pdf (532.4 KB)

Cooper - 2010 - Adding Liquid Payloads Effects to the 6-DOF Trajec.pdf (237.8 KB)

Conners - 1995 - Predicted Performance of a Thrust-Enhanced SR-71 A.pdf (912.6 KB)

Brumbaugh - 1991 - An aircraft model for the AIAA Controls Design Cha.pdf (970.6 KB)

Bowditch - AN EPITOME OF NAVIGATION.pdf (23.7 MB)

Bacon and Gregory - 2007 - General Equations of Motion for a Damaged Asymmetr.pdf (301.5 KB)

Antoniewicz et al. - User’s Manual for Interactive LINEAR, a FORTRAN Pr.pdf (4.3 MB)

An Energy Budget Model to Calculate the Low Atmosphere Profiles of Sound.pdf (962.8 KB)

Alderete - SIMULATOR AERO MODEL IMPLEMENTATION.pdf (67.9 KB)

A DISCUSSION OF METHODS OF REAL-TIME AIRPLANE FLIGHT SIMULATION.pdf (274.8 KB)

I don’t believe in the heliocentric earth. I read most the 1st of the 44 documents. US STANDARD OF ATMOSPHERE…

NOTE COPIED FROM DOC:
PAGE 6
For the accuracy required in this document, it suffices
to treat the surface = O as an ellipsoid whose
flattening (ellipticity) is
1.2.4- (13)
where b is the semiminor axis, or polar radius. It
should be noted that this value of the flattening is
the avera"'e value given in reference 8. In terms of
a and b the values To and 1/10 which correspond to
sea levei and ci> = 45° are found from the analytic
geometry of the ellipse to be:
1.2.4-(14)

PAGE 8
The meaning of geometric altitude Z and of
geopotential altitude H can be seen by reference to
figure 1.2.4(a). If Itn elementary plumb line is
used to explore gravity and if this plumb line is
rotating with the earth, then, starting at point 0
and proceeding outward, the little plumb line will
mark out line segments which progress along the
curved path OP. Under the influence of gravita-
tional and centrifugal forces this line OP will bend
polewards as it rises except along the axis of rotation
of the earth and along an equatorial radius extended

If we are going to fight for our beliefs we have no room for debate.