Multi-mode synchronized control for formation flying interferometer
This paper describes the design of an RCS based formation flying control for the Starlight space inteferometer mission, consisting of two spacecrafts.
formation flying control↗
Engineering topics
Lurie, B. J.
Publications and source records attributed to Lurie, B. J..
Vibration Attenuation Approach for Spaceborne Optical Interferometers
This paper proposes a vibration attenuation strategy for spaceborne optical interferometers to meet their sub-micron positional stability requirements.
Spaceborne↗
Asymptotically Globally Stable Multiwindow Controllers
The Popov criterion is applied to control system analysis and design. Nonlinear dynamic compensators (NDC) are introduced which ensure absolute stability without penalizing the available feedback.
Popov↗
Nonlinear Multi-Window Controllers
In many control designs the error signal is split into parallel channels which are tailored to be significant over distinct frequency ranges and are then recombined. Often, at least one channel contains nonlinear elements, The most common example is a PID controller with an anti-windup nonlinearity in the I-channel. A more general example using higher-order compensators is presented, which is a thermal controller for a spacecraft-mounted telescope.
PID↗
Integral Relations for Disturbance Isolation
Consider a system in Fig.1(a) of two bodies connected with an active strut (1) which is a linear motor.
mechanical↗
Design and implementation of active members for precision space structures
This paper describes the development and implementation of an active member in a precision truss structure. The active member utilizes a piezoelectric actuator motor imbedded in a steel case with built-in displacement sensor. This active member is used in structural quieting. Collocated active damping control loops are designed in order to impedance match piezoelectric active members to the structure. Results from application of these controllers and actuators to the JPL Phase B testbed are given.
Webster, M. S.↗
System identification and control of the JPL active structure
This paper describes recent advances in structural quieting technology as applied to active truss structures intended for high precision space based optics applications. Collocated active damping control loops are designed in order to impedance match piezoelectric active members to the structure. Noncollocated control loops are also studied in relation to controlling lightly damped structures.
Fanson, J. L.↗
Active suspensions for vibration isolation
The concept of mechanical impedances is used to analyze constraints on a single-link vibration isolation suspension. In particular, an assessment is made of the effects of the limited feedback bandwidth on the achievable suspension impedance and corresponding limits of attenuation of the transmitted force using Bode integral constraints and Blackman's formula. The performance of a piezoelectric strut is evaluated as an example.
Lurie, B. J.↗
Active member vibration control experiment in a KC-135 reduced gravity environment
An active member vibration control experiment in a KC-135 reduced gravity environment was carried out by the Air Force Flight Dynamics Laboratory and the Jet Propulsion Laboratory. Two active members, consisting of piezoelectric actuators, displacement sensors, and load cells, were incorporated into a 12-meter, 104 kg box-type test structure. The active member control design involved the use of bridge (compound) feedback concept, in which the collocated force and velocity signals are feedback locally. An impact-type test was designed to accommodate the extremely short duration of the reduced gravity testing window in each parabolic flight. The moving block analysis technique was used to estimate the modal frequencies and dampings from the free-decay responses. A broadband damping performance was demonstrated up to the ninth mode of 40 Hz. The best damping performance achieved in the flight test was about 5 percent in the fourth mode of the test structure.
Lawrence, C. R.↗
Multiloop Balanced Bridge Feedback in application to precision pointing
The Balanced Bridge Feedback technique is applied to the multiloop pointing control problem. Using colocated torque and angular velocity sensors and high-order compensators, the motor loop is decoupled from the flexible plant, the feedback bandwidth is increased in the motor and plant loops, and the accuracy improved by orders of magnitude compared to the results achievable with conventional control techniques.
Lurie, B. J.↗
Bridge feedback for active damping augmentation
A method is described for broadband damping augmentation of a structural system in which the active members (with feedback control) were developed such that their mechanical input impedance can be electrically adjusted to maximize the energy dissipation rate in the structural system. The active member consists of sensors, an actuator, and a control scheme. A mechanical/electrical analogy is described to model the passive structures and the active members in terms of their impedance representation. As a result, the problem of maximizing dissipative power is analogous to the problem of impedance matching in the electrical network. Closed-loop performance was demonstrated for single- and multiple-active-member controlled truss structure.
Chen, G.-S.↗
Experimental studies of adaptive structures for precision performance
An experimental study was made of the adaptive structure concept. Experimental data were obtained for a three-longeron, thirteen-bay truss-type test structure. This test structure can be softly suspended as well as rigidly clamped at the central bay. The load-carrying active member consists of a stack of concentric piezoelectric wafers, an eddy current displacement sensor, and a strain gage force sensor. A bridge (or compound) feedback technique developed in communication engineering is applied to the problem of active damping augmentation in adaptive structures. Using collocated force and velocity feedback around the active member, a desired output mechanical impedance can be implemented to maximize energy absorption by the active members. In addition, large gains can be implemented to linearize the active member's nonlinear behavior. Good agreements with linear finite element analysis was found for both static and dynamic structural responses. An 11 percent damping in the first bending mode was demonstrated in the closed-loop damping experiment.
Chen, G.-S.↗
Feedback maximization
Consideration is given to synthesis methods for feedback systems with nonlinear dynamic compensation, which permits increased feedback while preserving robustness, global stability, good transient responses, and stability of the output processes. Material needed for the realization of design goals from the areas of linear systems, nonlinear oscillation, and stability of nonlinear systems is covered. The three main parts of the book are: (1) linear feedback systems, (2) nonlinear feedback system analysis, and (3) synthesis methods for globally stable Nyquist-stable feedback systems with increased feedback.
Lurie, B. J.↗