https://i.ytimg.com/vi/D4AUYVnjMqI/hqdefault.jpg
For a printed version of my book in color, please go to LuLu:
http://www.lulu.com/spotlight/flat_earth
For a free PDF version, click on one of these links:
https://www.slideshare.net/secret/vDreJQ21p75q5Q
or
https://www.flatearthresearch.com/wp-content/uploads/2019/12/covered16emergencylandingsprovingflatearth-191007025918.pdf?fbclid=IwAR3R5b0rNaFiRmEWoQBPw7PjIT6q0rXqGRAdztCiYU8kK8zb5j-WDsGBIWc
Free high-resolution Gleason’s Map:
https://www.dropbox.com/s/9lcp65memq7vyxd/hi%20res%20restored%20gleason%20map.png?dl=0
“It’s flat & motionless Folks! From the Pilot’s basic study guide; please read 1.1.2 & let that sink in! Every Pilot was taught this, but some still don’t get it, (I didn’t at first) & some just stay asleep & yes it does say ‘assumed’ but when does the theory become a spinning reality? Where is the next part B manual to apply Coriolis & curvature nonsense to any flight? Never…because it is a flat & stationary Earth we live & fly on. All flight planning & aerial navigation is based always on a flat motionless plane! Curvature or spin is never accounted for EVER 😱☯️😴”
http://www.aerostudents.com/courses/flight-dynamics/flightDynamicsFullVersion.pdf
Flat nonrotating earth
page 126:
“The nonlinear equations of motion used are six-degree-of-freedom equations
sith stationary atmosphere and flat, nonrotating earth”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890007066.pdf
Determination of Angles of Attack and Sideslip from Radar Data and a Roll Stabilized Platform
NASA – March 1972 page 2:
“The method is limited, however, to application where a flat, nonrotating earth”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720012071.pdf
An Aircraft Model for the AIAA Controls Design Challenge
NASA – 1991 – page 11:
“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 non-rotating earth”
https://www.nasa.gov/centers/dryden/pdf/88248main_H-1777.pdf
Investigation of Aircraft Landing in Variable Wind Fields
NASA 1973 – page14 pdf or 6 on actual report:
a) The earth is flat and non-rotating.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790005472.pdf
A Mathematical Model of the CH-53 Helicopter
NASA – page 17:
“The helicopter equations of motion are given in body axes with rerpect to
a flat, nonrotating Earth.”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810003557.pdf
Atmospheric Oscillations
Georgia Tech April 1965
Prepared for NASA
page 13:
A model frequently used is that of a flat, nonrotating earth.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650015408.pdf
page 19:
These equations assume a rigid vehicle and a flat, nonrotating Earth.
https://www.nasa.gov/centers/dryden/pdf/88733main_H-2465.pdf
Flight Testing a VSTOL Aircraft
NASA 1988 – page 9 pdf or 4-5 on actual doc:
“For aircraft problems, the state and measurement models together represent the kinematics of a rigid body for describing motion over a flat, nonrotating Earth…”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880014378.pdf
Time to Climb
page2:
“In our minimum time-to-climb problem, the aircraft is modeled as a point mass and the flight trajectory is strictly
confined in a vertical plane on a non-rotating, flat earth.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060053337.pdf?
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