Neighboring optimal feedback control of multi- input nonlinear dynamical systems using discontinuous control
Neighboring optimal feedback control of multi-input nonlinear dynamic systems
Engineering topics
Publications and source records attributed to Fluegge-Lotz, I..
Neighboring optimal feedback control of multi-input nonlinear dynamic systems
Satellite feedback attitude control system resulting in high accuracy earth pointing motions in elliptic orbits
Optimal control method based on linear programming for satellite fuel consumption
Minimum fuel attitude control of spacecraft by Pontryagin principle and extended steepest descent method
Time function analysis for optimal control of satellite attitude and control jet fuel consumption in circular orbits
Time optimal control for nonlinear systems, expressing optimal control law as function of state variables
Nonlinear optimal attitude control of planet pointing space vehicles, and optimal control of satellite trajectories
Control systems for high accuracy earth pointing attitude motions of satellite configurations in elliptic orbits
Satellite attitude control in elliptic orbit
Attitude control for earth satellite in elliptic orbit, linearization in attitude control, and computation of optimal controls by method based on second variations
Time-optimal control problem studied for system representing second-order nonlinear differential equation
Attitude control system for satellite in elliptical orbit calculated by linear equations and computer simulation
Minimum fuel control of spacecraft in orbit using extended method of steepest descent
Spinning space vehicle and satellite attitude stabilization using contactor control system with linear switching surface, comparing with time- optimal solutions
Minimum effort restoration of perturbed system to equilibrium state defined as time varying function of instantaneous state of system
Pontryagin optimal principle applied to minimum fuel satellite attitude control with two feedback controls
So-called flip-flop controls (also called "on-off-course controls") are frequently preferred to continuous controls because of their simple construction. Thus they are used also for the steering control of airplanes. Such a body possesses-even if one thinks, for instance, only of the symmetric longitudinal motion - three degrees of freedom so that a study of its motions under the influence of an intermittent control is at least lengthy. Thus, it is suggested that an investigation of the basic effect of such a control first be made on a system with one degree of freedom. Furthermore, we limit ourselves in the resent report to the investigation of an "ideal" control where the control surface immediately obeys the command given by the "steering control function". Thus the oscillation properties of the control surface and the defects in linkage, sensing element, and mixing device are, at first, neglected. As long as the deviations from the "ideal" control may be neglected in practice, also the motion of the control surface takes place at the heat of the motion of the principal system. The aim of our investigation is to obtain a survey of the influence of the system and control coefficients on the damping behavior which is to be attained.