The problem to be solved, as presented to the pilot or observer of an aircraft, is as follows: The aircraft starting from A must land at B, the only data being the speed of the airplane, the altitude and the orientation D of the course. The above data would be amply sufficient, were it not for the fact that the airplane is constantly subjected to a wind of variable direction and strength.
Aerial navigation by dead reckoning
Congres International de la Navigation Aerienne (1st : 1921 : Paris, France)
1922-07-01
Miscellaneous
No indication
English
The importance of dead reckoning in aerial navigation
Engineering Index Backfile | 1929
|Dead reckoning navigation equations
NTRS | 1970
Unmanned aerial vehicle navigation verification system based on dead reckoning
European Patent Office | 2024
|GPS Aided Dead Reckoning Navigation
British Library Conference Proceedings | 1994
|Dead Reckoning Navigation for Walking Robots
NTIS | 1991
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