This chapter contains sections titled:
Trim
Treatment of Stability and Control
Static Stability
Dynamic Stability
Hingeless Rotor
Control
Autostabilization
References
Trim, Stability and Control
2011-07-29
13 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
trim, stability and control , balance of moments, aircraft centre of gravity (CG) ‐ attitude, adopted by airframe , system design, degree of augmentation desired ‐ and total control power , static and dynamic stability ‐ flying qualities of helicopter , flight principle, of any aircraft ‐ aerodynamic, gravitational forces and moments, in balance , yawing moment balance ‐ by tail rotor thrust selection , mathematical treatment of dynamic stability ‐ by Bramwell, standard treatment , pitch attitude, airframe in flight ‐ balance of pitching moments, about CG , autostabilization, response to situation ‐ inadequate basic stability and ample control power , fuselage attitude in forward flight ‐ forward CG, aft CG, forward CG with direct head moment
TRIM-STAB-Aerospace vehicle trim and stability
NTRS | 1977
|Flight control stability and trim analysis techniques
AIAA | 1982
|Trim and Longitudinal Stability
Springer Verlag | 2018
|TRIM ANGLE CONTROL APPARATUS AND TRIM ANGLE CONTROL METHOD
Europäisches Patentamt | 2024
|