Add to ORKGThe development of an advanced, computerized method for the analysis and evaluation of the aeroelastic stability and control parameters of controls fixed and controls free flight vehicles is presented. Specifically, the Level 2.01 FLEXSTAB computer program system is described. Technical areas in aerodynamics, dynamics, and control system synthesis are defined in which further research and development are planned to extend the analysis capability of the system for future CCV applications
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
The work contained in this report is part of an on-going programme of research into handling qualiti...
A review of analytical methods and associated tools for active controls analysis and design problems...
The design of modern aerospace systems relies on the efficient utilization of computational resource...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
Recently completed B-52 Control Configured Vehicles (CCV) flight testing is summarized, and results ...
A survey of the stability analysis techniques for automatically controlled aircraft is presented. Th...
With many modern fighter aircraft experiencing unpredicted flight dynamics during flight tests, rece...
Values of plant dynamic uncertainties for some recent aircraft design and development programs are g...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
An effort to develop techniques for the design of integrated, fully automatic flight control systems...
In the aviation industry, aircraft manufactures are constantly striving to fully understand the esse...
Testing and evaluation of a stability augmentation system for aircraft flight control were performed...
A set of digital flight control laws were designed for the NASA F-8C digital fly-by-wire aircraft. T...
A computer program for determining the flight characteristics of light aircraft was developed. The p...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
The work contained in this report is part of an on-going programme of research into handling qualiti...
A review of analytical methods and associated tools for active controls analysis and design problems...
The design of modern aerospace systems relies on the efficient utilization of computational resource...
Despite significant advancements in controls configured vehicles/active controls technology (CCV/ACT...
Recently completed B-52 Control Configured Vehicles (CCV) flight testing is summarized, and results ...
A survey of the stability analysis techniques for automatically controlled aircraft is presented. Th...
With many modern fighter aircraft experiencing unpredicted flight dynamics during flight tests, rece...
Values of plant dynamic uncertainties for some recent aircraft design and development programs are g...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
An effort to develop techniques for the design of integrated, fully automatic flight control systems...
In the aviation industry, aircraft manufactures are constantly striving to fully understand the esse...
Testing and evaluation of a stability augmentation system for aircraft flight control were performed...
A set of digital flight control laws were designed for the NASA F-8C digital fly-by-wire aircraft. T...
A computer program for determining the flight characteristics of light aircraft was developed. The p...
The potential effects of fly by wire and control configured vehicle concepts on flying qualities are...
The work contained in this report is part of an on-going programme of research into handling qualiti...
A review of analytical methods and associated tools for active controls analysis and design problems...