Equations of motion of aerospace vehicles with various arrangements of wings and control surfaces are discussed. The equations devised are complete descriptions of the systems and can therefore be reduced to a system of transfer functions and control diagrams that take account of interactions of the various parts of the vehicle. The dynamic characteristics of the vehicles are presented for standard input disturbances, which are represented in the form of Laplace and z-transforms. A matrix form of description of the vehicle is proposed as a means of taking account of the nonstationary nature of the controlled object. These characteristics make it possible to identify the object on the basis of experimental data. (Author)
Aerospace Vehicles as Objects of Control
1974
209 pages
Report
Keine Angabe
Englisch
Aerospace vehicles as objects of control
TIBKAT | 1974
|Guidance and control of aerospace vehicles
TIBKAT | 1963
|Aerospace vehicles and adaptive flight control
Engineering Index Backfile | 1962
|Control synthesis for spinning aerospace vehicles.
NTRS | 1967
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