Add to ORKGA method to evaluate the lateral ride quality of a B-1 aircraft subjected to a reduction in lateral static stability is developed. Ride quality is then found for three different relaxed static stability configurations which are augmented by yaw rate feedback to restore specified handling qualities. These cases are compared to the ride quality of the unrelaxed aircraft with the same handling qualities
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
This report presents the results of an analytical study of the lateral controllability of an airplan...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle
State variable techniques are utilized to generate the RMS vertical load factors for the B-52H and B...
The RQ trends which large flexible aircraft exhibit under various parameterizations of control laws ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering."Dec...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
To improve the ride quality in short takeoff aircraft, several means have been investigated. In gene...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
An investigation has been made in the Langley free-flight tunnel to determine the low-speed static l...
Data are presented showing compliance of C-54D with Army and Navy lateral and directional stability ...
The blended-wing-body (BWB) configuration appears as a promising contender for the next generation o...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
This report presents the results of an analytical study of the lateral controllability of an airplan...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle
State variable techniques are utilized to generate the RMS vertical load factors for the B-52H and B...
The RQ trends which large flexible aircraft exhibit under various parameterizations of control laws ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering."Dec...
The effects on dynamic lateral stability and controllability of some of the important aerodynamic an...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
To improve the ride quality in short takeoff aircraft, several means have been investigated. In gene...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
An investigation has been made in the Langley free-flight tunnel to determine the low-speed static l...
Data are presented showing compliance of C-54D with Army and Navy lateral and directional stability ...
The blended-wing-body (BWB) configuration appears as a promising contender for the next generation o...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The results of a number of recent lateral-stability investigations conducted by the NACA are summari...
This report presents the results of an analytical study of the lateral controllability of an airplan...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle