An investigation of the feasibility of obtaining lateral stability derivatives for a linear aircraft by matching analog computer transient responses to flight test data
Main Authors: | Adams, R. C., Dedman, T. F., Cooper, C. R. |
---|---|
Other Authors: | Dept. of Aeronautical Engineering |
Language: | en_US |
Published: |
Princeton, New Jersey : Princeton University
2012
|
Online Access: | http://hdl.handle.net/10945/14322 |
Similar Items
-
Transient aerodynamics effect on v-tail aircraft in lateral stability
by: Musa, Nur Amalina
Published: (2017) -
An investigation of a method for unique determination of aircraft longitudinal stability derivatives from transient flight test data
by: Cornwell, R. R., et al.
Published: (2012) -
The Feasibility of Remotely Piloted Aircrafts for VOR Flight Inspection
by: Diogo de Oliveira Costa, et al.
Published: (2020-03-01) -
Double Rotational Flight of an Aircraft: A Feasibility Study
by: Pei-MinTsai, et al.
Published: (2012) -
The instrumentation of the S-2 aircraft for stability and control flight testing.
by: Duncan, Thomas John
Published: (2012)