Många har tagit det som sin uppgift att plöja genom mängder av dokument för att hitta bevisen på de uppgifter som presenteras till oss gällande vår värld. Vare sig man är en anhängare av NASA eller har vaknat upp till bedrägeriet, vill det som är skrivet vara en beskrivning som antigen bekräftar eller förkastar en teori.
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I alla dokument beskrivs jorden på samma sätt, här är några korta statements:
1. Jorden är en platt yta.
2. Jorden står stilla.
3. Solen rör sig över jorden.
4. Solen är nära, i vår egen atmosfär, inte 150 miljoner km borta.
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Jag lägger upp ett klipp för den som vill titta på en sammanfattning, men nedan kommer jag också fylla på med länkar efterhand som jag får nya i min besittning: på så vis är det dokumenterat, du kan själv följa länkarna och behöver inte ta din information från en tredje part.
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Detta är offentliga dokument. Någon har gjort grundjobbet, allt vi behöver ä att läsa vad som faktiskt är skrivet. Jag har gjort notat vid några av filerna.
Länkar är skrivna under texterna så man själv kan gå in via deras egna hemsidor, men jag har också länkat direkt till PDF filerna där det är möjligt. Enjoy!
Jorden är platt - välkommen till verkligheten!
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Klicka på PDF symbolerna för att själv läsa
NASA's Reference Publication 1207, augusti 1988
Derivation and Definition of a Linear Aircraft Model ( augusti 1988)
https://nasa.gov/centers/dryden/pdf/88104main_H-1391.pdf
Textexempel:
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. Återfinns under Summary
* Summary, sida 6
* Introduction, sida 6, #2
* Concluding Remarks, sida 30
* Report Document Page, #16, sida 102
Dokument 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
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Textexempel:
In this paper, the rigid body equations of motion over a flat non-rotating earth are developed...
* Sida 2, #2
NASA Technical Memorandum 104330, juni 1997
Predicted Performance of a Thrust-Enhanced SR71 Aircraft with an External Payload
https://www.nasa.gov/centers/dryden/pdf/88507main_H-2179.pdf
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Textexempel:
The DPS equations of motion use four assumptions... a nonrotating Earth.
* Digital Performance Simulation Description Sida 10 (sida 8 i rapporten)
NASA Technical Note 19710018599, juni 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
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Textexempel:
A flat, nonrotating Earth.
* Problem Statement, sida 14 (sida 12 i rapporten)
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
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Textexempel:
This simulation assumes...the missile position in space is computet relative to a flat nonrotating Earth.
* Trajectory Simulation, sida 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
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Textexempel:
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, sida 16, #3 (sida 12 i rapporten)
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
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Textexempel:
The nonlinear equations of motion used are six-degree-of-freedom equations with stationary atmosphere and flat, nonrotating earth assumptions.
* Summary, sida 4
* Report Documentation Page, sida 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
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Textexempel:
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, sida 13 (sida 11 i rapporten)
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
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Textexempel:
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, sida 14 (sida 6 i rapporten)
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
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Textexempel:
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.
* Sida 13 ( sida 10 i rapporten)
NASA Technical Memorandum 81238, novebmer 1980
A Mathematical Model of the CH-53 Helicopter
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810003557.pdf
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Textexempel:
The helicopter equations of motion are given in body axes with respect to a flat, nonrotating Earth.
* Equations of Motion, sida 25 (sida 17 i rapporten)
NASA Technical Paper 2002-210718, juni 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
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Textexempel:
These equations assume a rigid vehicle and a flat, nonrotating Earth.
* Equations of Motion, 18-19 (sida 10-11 i rapporten)
NASA Technical Memorandum 100996, maj 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
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Textexempel:
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, sida 8-9 (sida 4-5 i rapporten)
NASA Ames Research Center, januari 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
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Textexempel:
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, sida 2
NASA Technical Memorandum, mars 1972
Determination of Angles of Attack and Sideslip from Radar Data and a Roll Stabilized Platform
https://ntrs.nasa.gov/citations/19720012071
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Textexempel:
The method is limited, however, to application where a flat, nonrotating earth may be assumed.
* Sida 2 #16
CIA-RDP86-00513R001343720008-3, december 1967
Scientific Abstract Pyaskovskaya-Fesenkova, YE.V.-
https://www.cia.gov/readingroom/document/cia-rdp86-00513r001343720008-3
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Väljer att inte skriva kommentarer här, länkarna finns både till myndighetens "readingroom" och direkt till PDFfilen.
"Den som har ögon må se..."
Tips: himlavalvet!
P 1386-B
United States Geological Survey
Professional Paper 1386-B
https://pubs.usgs.gov/pp/p1386/
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Av speciellt intresse:
P 1386-B: Antarctica (1988)
P 1386-D: Iceland
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