A technique is described which can be used for design of feedback controllers for high-performance aircraft operating in flight conditions in which nonlinearities significantly affect performance. Designs are performed on a mathematical model of the longitudinal dynamics of a hypothetical aircraft similar to proposed supermaneuverable flight test vehicles. Nonlinear controller designs are performed using truncated solutions of the Hamilton-Jacobi-Bellman equation. Preliminary results show that the method yields promising results.
Nonlinear longitudinal control of a supermaneuverable aircraft
1989 American Control Conference ; 1989 ; Pittsburgh, PA, United States
1989-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Nonlinear control of a supermaneuverable aircraft
NTRS | 1989
|Nonlinear control of a supermaneuverable aircraft
AIAA | 1989
|