A method to derive angle of pitch, flight-path angle and angle of attack from measurements in nonsteady flight
1971
105 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Optimal perturbation guidance with constraints on terminal flight-path angle and angle of attack
SAGE Publications | 2019
|Aircraft flight path angle display system
NTRS | 1991
|