CONTROLLERS FOR SPACE STRUCTURES

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$442,000.00
Award Year:
1989
Program:
SBIR
Phase:
Phase II
Contract:
n/a
Agency Tracking Number:
6523
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Techno-sciences
7833 Walker Dr - Ste 308, Greenbelt, MD, 20770
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
William H Bennett
(301) 345-1692
Business Contact:
() -
Research Institution:
n/a
Abstract
THE UNPRECEDENTED POINTING AND TRACKING ACCURACIES REQUIRED IN STRATEGIC DEFENSE ENGAGEMENT SCENARIOS PRESENT FORMIDABLE CHALLENGES TO THE DESIGNERS OF PLATFORM CONTROL SYSTEMS FOR SLEWING AND VIBRATIONSUPPRESSION. IT IS CLEAR THAT CONVENTIONAL DESIGN PROCEDURES BASED ONFINITE DIMENSIONAL, LUMPED PARAMETER MODELS (FINITE ELEMENTS OR MODES)ARE INADEQUATE TO THE TASK. ADVANCED DESIGN METHODS ARE BEING DEVELOPED FOR MODELING AND CONTROL OF FLEXIBLE STRUCTURES. THESE METHODS HAVE THE ANALYTICAL SOPHISTICATION TO TREAT THE VIBRATION SUPPRESSION PROBLEM IN THE DETAIL NECESSARY TO CAPTURE ALL FACTORS RELEVANT TO ACCURATE POINTING REQUIREMENTS. DIRECTIONS EXPLORED IN PREVIOUS WORK ARE BEING DEVELOPED AND EXPANDED TO THE LEVEL THAT SIGNIFICANT ENGINEERING EVALUATION OF CONTROLLERS FOR REALISTIC SPACE STRUCTURE PROBLEMS CAN BE DESIGNED.

* information listed above is at the time of submission.

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