Multivariable adaptive surface control

• US 5,374,011 A
• Filed: 11/13/1991
• Issued: 12/20/1994
• Est. Priority Date: 11/13/1991
• Status: Expired due to Fees

• Current Assignee: Massachusetts Institute of Technology
• Original Assignee: Massachusetts Institute of Technology
• Inventors: Lazarus, Kenneth B., Crawley, Edward F.
• Primary Examiner(s): Focarino, Margaret A.
• Assistant Examiner(s): Ellis, Christopher P.
• Application Number:
  US07/791,899
• Time in Patent Office: 1,133 Days
• Field of Search: 244/75 R, 244/75 A, 244/76 C, 244/76 R, 244/195, 244/198, 244/200, 244/201, 244/220, 244/221, 244/228, 310/800, 310/328, 310/326
• US Class Current: 244/99.8
• CPC Class Codes: B64C 3/48 by relatively-movable parts of wing structures
• CPC Class Codes: B64G 1/22 Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
• CPC Class Codes: B64G 1/36 using sensors, e.g. sun-sensors, horizon sensors
• CPC Class Codes: G05D 1/0825 using mathematical models

Abstract

An adaptive sheet structure with distributed strain actuators is controlled by a dynamic compensator that implements multiple input, multiple output control laws derived by model-based, e.g., Linear Quadratic Gaussian (LQG) control methodologies. An adaptive lifting surface is controlled for maneuver enhancement, flutter and vibration suppression and gust and load alleviation with piezoceramic elements located within, or enclosed by sheets of composite material at a particular height above the structure'"'"'s neutral axis. Sensors detect the amplitudes of lower order structural modes, and distributed actuators drive or damp these and other modes. The controller is constructed from an experimental and theoretical model using conventional control software, with a number of event recognition patterns and control algorithms programmed for regulating the surface to avoid instabilities. The number of control states of the compensator is then reduced by removing states having negligible effects on the plant, and a smaller set of control laws are optimized and then adjusted based on analytical models bench and wind-tunnel testing.

Claims

1. A system controlling disturbances and instabilities in a sheet structure having a surface contacting a surrounding fluid and dynamically interacting therewith, such system comprising

a plurality of m actuators attached to the sheet structure, each actuator being located to couple energy into a control segment consisting of a region of said sheet structure about such actuator,

a multi-channel amplifier having a plurality of n power outputs for separately driving ones of the m actuators,

a plurality of s sensors located with respect to said sheet structure for sensing physical parameters associated with dynamics of the sheet structure and for producing sensing signals indicative thereof, m, n and s being positive integers,

estimator means for receiving said sensing signals and determining therefrom estimated state variables descriptive of behavior of said sheet structure, and

control means operative on ones of said sensing signals and on at least some of said estimated state variables for producing control outputs, said control outputs controlling the multi-channel amplifier to drive selected ones of the actuators with an amplitude to control a dynamic physical condition of said sheet structure.

2. A system according to claim 1, wherein the control means includes a processor that implements a state machine having machine states corresponding to states of said sheet structure, control states corresponding to processes for altering the machine states, and selecting means determined by said machine states and said control states for driving the selected ones of the actuators to achieve suppression or alleviation of an unwanted response of the sheet structure.

3. A system according to claim 1, wherein the sheet structure is a composite wing having an outside bounding surface, and said actuators are enclosed by said outside bounding surface.

4. A system according to claim 3, wherein the composite wing has an inside bounding surface, and said actuators are embedded between the inside bounding surface and the outside bounding surface.

5. A system according to claim 2, wherein said estimated state variables determined by said estimator means include amplitudes of lower order structural modes of said sheet structure or a combination thereof.

6. A system according to claim 5, wherein sensed physical parameters include at least one of temperature, surrounding fluid speed, pressure, structure displacement, strain, acceleration and strain rate.

7. A system according to claim 3, wherein a control law causes the actuators to transfer strain to the sheet structure in a manner to decrease load on the composite wing and produce gust alleviation.

8. A system according to claim 6, wherein the sheet structure is an outer fluid-contacting surface of a vessel hull.

9. A system according to claim 6, wherein the sheet structure is a sail.

10. A system according to claim 5, wherein the sheet structure is a panel.

11. A system according to claim 2, wherein some of said actuators are arranged to couple strain energy into regions of said sheet structure to excite bending and torsional modes of the structure.

12. A system according to claim 11, wherein the sheet structure extends from a root attached to a vessel, and said control means includes control laws for driving some of said actuators to decrease loading on the root.

13. A system according to claim 6, wherein the sheet structure is a vessel fuselage.

14. A system according to claim 5, wherein the sheet structure is an antenna.

15. A controllable sheet structure comprising a skin of a first material having a surface in contact with a surrounding fluid and in dynamic interaction therewith, and at least one actuator of a second material attached to said structure for coupling strain energy over a region into said structure, wherein mechanical impedance of each said actuator is matched to stiffness of said structure over the region to optimize coupling of strain energy thereto, and a dynamic compensator operative on sensed physical parameters of said structure for determining state variables and producing control outputs, said control outputs controlling outputs of a multi-channel amplifier in accordance with the determined state variables to drive selected ones of the actuators with an amplitude to control a dynamic physical condition of said sheet structure.