NASA FLAT EARTH DOCUMENTS
NASA along with Navy, Army, Flight schools all state that assumptions have to be made with aircraft.
Are they assuming the earth is a ball with a 8 inches per mile (or miles squared) ?
Nope! Why not? Because if they did, the pilots would have to constantly dip down to compensate for vertical drop in every direction and crash the aircraft HAHAHHA.
What does assumption mean? a thing that is accepted as true or as certain to happen, without proof. – Oxford Dictionary
General Equations of Motion for Damaged Asymmetric Aircraft
Page 1: “…equations of motions must properly reflect the underlying physics.”
page 2:
“In this paper, the rigid body equations of motion over a flat
non-rotating earth are developed…”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20070030307.pdf
Approximate Optimal Guidance for the Advanced Launch System
On page one this document does mention a spherical rotating earth but then states that “…these schemes” (based on a spherical rotating earth) 1) “…are difficult to prove” and 2) “…not suggested to be used as a basis for an online real-time guidance law.”
Page 32 goes on to say:
“Lastly, the equations of motion for the zeroth-order problem of flight in a vacuum over a flat Earth are presented.”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940020279.pdf
SR-71
Page 8 “…nonrotating Earth…”
https://www.nasa.gov/centers/dryden/pdf/88507main_H-2179.pdf
page 14:
/pdf/88072main_H-1259.pdf
NASA Technical Paper 2835
Page 1 Summary:
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
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 nonrotating 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 respect to
a flat, nonrotating Earth.”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810003557.pdf8
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
Russia 1948
Shape of the earth unknown..
https://www.cia.gov/library/readingroom/docs/CIA-RDP80-00809A000600231031-1.pdf
Russian Light Study
“Brightness of the firmament”
Flat earth :
https://drive.google.com/file/d/1KX7_0tlTAzFEWJ1CWOXQ_K2JnUgbfzb8/view
Propagation of Electromagnetic Fields Over Flat Earth
http://www.arl.army.mil/arlreports/2001/ARL-TR-2352.pdf
page 9: based upon the signal having a single bounce on a flat Earth
http://www.arl.army.mil/arlreports/2009/ARL-TR-4998.pdf
page 1:
Trajectory of Spinning Projectiles:
“These equations assume a flat Earth.”
http://www.arl.army.mil/arlreports/2010/ARL-TR-5118.pdf
page 2:
“These equations assume a flat Earth..”
http://www.arl.army.mil/arlreports/2011/ARL-TR-5810.pdf
page 216:
“assuming a flat Earth“
http://tycho.usno.navy.mil/ptti/2007papers/paper21.pdf
Page 1:
“…so that a flat-earth approximation provides the best estimate.”
http://www.arl.army.mil/arlreports/2001/ARL-TN-175.pdf
Page 39:
model works over a flat earth
http://www.arl.army.mil/arlreports/2003/ARL-TR-2696.pdf
page 1:
transmission loss over flat earth
http://www.arl.army.mil/arlreports/2000/ARL-TR-2156.pdf
page 9:
“…input to a flat earth”
http://www.arl.army.mil/arlreports/2003/ARL-MR-563.pdf
page 3:
“The first is the Earth-fixed coordinate system, which is fixed to the Earth with a flat Earth assumption.”
http://www.arl.army.mil/arlreports/2010/ARL-CR-650.pdf
page: 1
flat earth approximation provides the best estimate
http://www.arl.army.mil/arlreports/2002/ARL-TR-2683.pdf
page 32:
This model works well over a flat-earth
http://www.arl.army.mil/arlreports/2000/ARL-TR-1812.pdf
page 168:
equations of flat-earth trigonometry.
http://www.irig106.org/docs/106-17/106-17_Telemetry_Standards.pdf
page 8:
The Earth is flat and nonrotating.
http://www.navair.navy.mil/nawcwd/command/Inplace.aspx/LoadFile/531