Anti-Disinformation

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890007066.pdf
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/citations/19720012071

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/citations/19720012071

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/citations/19790005472

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/citations/19810003557

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/citations/19650015408

page 19:
These equations assume a rigid vehicle and a flat, nonrotating Earth.
https://www.nasa.gov/centers/dryden/p...

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/citations/19880014378

https://www.nasa.gov/centers/dryden/pdf/88733main_H-2465.pdf

Time to Climb
https://ntrs.nasa.gov/citations/19880014378
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/citations/20060053337

ntrs.nasa.gov

User's manual for interactive LINEAR: A FORTRAN program to derive linear aircraft models - NASA Technical Reports Server (NTRS)

An interactive FORTRAN program that provides the user with a powerful and flexible tool for the linearization of aircraft aerodynamic models is documented in this report. The program LINEAR numerically determines a linear system model using nonlinear equations…

927 viewsShane St. Pierre, 18:58

35 Times NASA/CIA/FAA Documents REFER to '... over a flat, non-rotating earth”

35 Government Documents Admit Flat Earth NASA, ARMY, FAA, AIR FORCE, CIA
https://youtu.be/_dcK5q6N3lU

Singapore/New York/Singapore flights SQ21/SQ22 - More proofs of a FLAT EARTH
https://youtu.be/D4AUYVnjMqI

If the earth is a spinning globe (oblate spheroid) in the infinite vacuum of space then why does NASA in “NASA Reference Publication 1207 – August 1988” on page 30, refer to a “a stationary atmosphere over a flat, non-rotating earth”?

Flight Dynamics Summary
http://www.aerostudents.com/courses/flight-dynamics/flightDynamicsFullVersion.pdf

"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 😱☯️😴"

730 viewsShane St. Pierre, 19:00

Anti-Disinformation

Forwarded from Smoke and Mirrors

WARNING - GRAPHIC - Vaccine Carnage In The ER , a nurse speaks out (VIEWER DISCRETION ADVISED)

535 viewsSmoke and Mirrors, 19:36

Anti-Disinformation

Flight Dynamics Summary.pdf

412.7 KB

User's_manual_for_interactive_LINEAR_A_FORTRAN_program_to_derive.pdf

4.3 MB

Determination_of_angles_of_attack_and_sideslip_from_radar_data_and.pdf

1.3 MB