Many have taken it upon themselves to plow through lots of documents in search of the actual presentation made by these organisations about our world. Whether you are a fan of NASA or you are aware of the deception; their written description will confirm or discard whichever theory you may have.
All these documents describes the earth in the same manner, here are a few statements:
1. The earth is a flat surface.
2. The earth is not moving.
3. The sun is moving above the earth.
4. The sun is close, within our atmosphere, not 93 millions miles away.
These are public records. Someone has done the groundwork, all you have to do is take the time to look up what is actually written. I have made some notes along some of the files.
I have included the links, but you can also go directly by the PDF files. Enjoy!
The earth is flat - welcome to the reality!
Klick on the PDF symbol and read for yourself...
NASA's Reference Publication 1207, August 1988
Derivation and Definition of a Linear Aircraft Model ( augusti 1988)
https://nasa.gov/centers/dryden/pdf/88104main_H-1391.pdf
Text-example:
This report documents the derivation and definition of a linear aircraft model for a rigid aircraft of constant mass flying over a flat, nonrotating Earth. Found under Summary.
* Summary, page 6
* Introduction, page 6, #2
* Concluding Remarks, page 30
* Report Document Page, #16, page102
Document 20070030307
American Institute of Aeronautics and Astronautics
General Equations of Motion for a Damaged Asymmetric Aircraft.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20070030307.pdf
Text-example:
In this paper, the rigid body equations of motion over a flat non-rotating earth are developed...
* Page 2, #2
NASA Technical Memorandum 104330, June 1997
Predicted Performance of a Thrust-Enhanced SR71 Aircraft with an External Payload
https://www.nasa.gov/centers/dryden/pdf/88507main_H-2179.pdf
Text-example:
The DPS equations of motion use four assumptions... a nonrotating Earth.
* Digital Performance Simulation Description, Page 10 (page 8 in the report)
NASA Technical Note 19710018599, June 1971
A Method for Reducing The Sensitivity of Optimal Nonlinear Systems to Parameter Uncertainty
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710018599.pdf
Text-example:
A flat, nonrotating Earth.
* Problem Statement, Page 14 (page 12 in the report)
NASA Technical Note 20040008097, April 1961
Calculation of Wind Compensation for Launching of unguided Rockets
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20040008097.pdf
Text-example:
This simulation assumes...the missile position in space is computet relative to a flat nonrotating Earth.
* Trajectory Simulation, Page 8 #2
NASA Technical Paper 2768, December 1987
User's Manual for LINEAR, a FORTRAN program to Derive Linear Aircraft Models
https://www.nasa.gov/centers/dryden/pdf/88072main_H-1259.pdf
Text-example:
Within the program, the nonlinear equations of motion include 12 states representing a rigid aircraft flying in a stationary atmosphere over a flat nonrotating Earth.
* Program Overview, Page 16, #3 (page 12 in the report)
NASA Technical Paper 2835, September 1988
User's Manual for LINEAR, a FORTRAN Program to Derive Linear Aircraft Models
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890007066.pdf
Text-example:
The nonlinear equations of motion used are six-degree-of-freedom equations with stationary atmosphere and flat, nonrotating earth assumptions.
* Summary, Page 4
* Report Documentation Page, Page 126 # 16
NASA Contractor Report 186019, December 1991
An Aircraft Model for the AIAA Controls Design Challenge
https://www.nasa.gov/centers/dryden/pdf/88248main_H-1777.pdf
Text-example:
The nonlinear equations of motion used in this model are general six-degree-of-freedom equations representing the flight dynamics of a rigid aircraft flying in a stationary atmosphere over a flat nonrotating Earth.
* Equations of Motion and Atmospheric Model, Page 13 (page 11 in the report)
NASA Contractor Report 3073, December 1978
Investigation of Aircraft Landing in Variable Wind Fields
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790005472.pdf
Text-example:
The Aircraft trajectory model employed in this study was derived based on the following assumptions: a) The Earth is flat and nonrotating.
* Chapter II - Aircraft Landing Model, Page 14 (page 6 in the report)
Engineering Experiment Station, Georgia Institute of Technology, Prepared for NASA; April 1965
Atmospheric Oscillations
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650015408.pdf
Text-example:
A model frequently used is that of a flat, nonrotating earth.
The most one can profitably simplify the problem is to consider an isothermal atmosphere, plane level surface, and a nonrotating Earth.
* Page 13 ( page 10 in the report)
NASA Technical Memorandum 81238, November 1980
A Mathematical Model of the CH-53 Helicopter
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810003557.pdf
Text-example:
The helicopter equations of motion are given in body axes with respect to a flat, nonrotating Earth.
* Equations of Motion, Page 25 (page 17 in the report)
NASA Technical Paper 2002-210718, June 2002
Stability and Control Estimation Flight Test Results for the SR-71 Aircraft with Externally Mounted Experiments
https://www.nasa.gov/centers/dryden/pdf/88733main_H-2465.pdf
Text-example:
These equations assume a rigid vehicle and a flat, nonrotating Earth.
* Equations of Motion, Pages 18-19 (pages 10-11 in the report)
NASA Technical Memorandum 100996, May 1988
Flight Testing a VSTOL Aircraft to Identify a Full-Envelope Aerodynamic Model.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880014378.pdf
Text-example:
For aircraft problems, the state and measurements models together represent the kinematics of a rigid body for describing motion over a flat, nonrotating Earth.
* State Estimation, Pages 8-9 (pages 4-5 in the report)
NASA Ames Research Center, January 2006
Singular Arc Time-Optimal Climb Trajectory of Aircraft in a Two-Dimensional Wind Field
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060053337.pdf
Text-example:
In our minimum time-to-climb problem, in aircraft is modeled as a point mass and the flight trajectory is strictly confined in a vertical plane on a non-rotating, flat Earth.
* Singular Arc Optimal Control, Page 2
NASA Technical Memorandum, March 1972
Determination of Angles of Attack and Sideslip from Radar Data and a Roll Stabilized Platform
https://ntrs.nasa.gov/citations/19720012071
Text-example:
The method is limited, however, to application where a flat, nonrotating earth may be assumed.
* Page 2 #16
CIA-RDP86-00513R001343720008-3, December 1967
Scientific Abstract Pyaskovskaya-Fesenkova, YE.V.-
https://www.cia.gov/readingroom/document/cia-rdp86-00513r001343720008-3
I choose not to make comments here - follow the links to the governments "readingroom" and directly via the PDF file.
"Those who have eyes..."
Keyword: the firmament!
P 1386-B
United States Geological Survey
Professional Paper 1386-B
https://pubs.usgs.gov/pp/p1386/
These might be of special interest:
P 1386-B: Antarctica (1988)
P 1386-D: Iceland