Basic operating principle of adaptive control function is that sums of properly modulated, conventional linear feedback and feedforward signals provide control inputs needed to obtain specified responses in number of output variables of linear controlled element; adaptive control function approach is applied to design of adaptive, lateral stability augmentation system for hypothetical, manned, lifting-body, entry vehicle; objective of application is to effect considerable improvement in lateral-directional handling qualities of vehicle; data from simulation of system demonstrate its effectiveness. (06891)
New methods in adaptive flight control
NASA CR
NASA Contractor Reports ; n 1152
1968
134 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
In Flight Validation of Adaptive Flight Control Methods
AIAA | 2008
|In Flight Validation of Adaptive Flight Control Methods
British Library Conference Proceedings | 2008
|New methods in adaptive flight control
NTRS | 1968
|Adaptive Methods for Flight Control Diagnostics
British Library Conference Proceedings | 2008
|New Methods in Adaptive Flight Control
NTIS | 1968
|