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THE MISSILE AUTOPILOT DESIGN PROBLEM IS A NONLINEAR TIME VARYING STOCHASTIC…

Award Information

Agency:
Department of Defense
Branch:
Air Force
Award ID:
4364
Program Year/Program:
1986 / SBIR
Agency Tracking Number:
4364
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Scientific Systems Company, Inc
500 West Cummings Park - Ste 3000 Woburn, MA -
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Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 1986
Title: THE MISSILE AUTOPILOT DESIGN PROBLEM IS A NONLINEAR TIME VARYING STOCHASTIC CONTROL PROBLEM.
Agency / Branch: DOD / USAF
Contract: N/A
Award Amount: $59,955.00
 

Abstract:

THE MISSILE AUTOPILOT DESIGN PROBLEM IS A NONLINEAR TIME VARYING STOCHASTIC CONTROL PROBLEM. PREVIOUS APPROACHES BASED ON EITHER CLASSICAL DESIGN OR LINEAR MULTIVARIABLE DESIGN HAVE PROVIDED INDEQUATE FOR THE NEW GENERATION OF HIGHLY MANEUVERABLE AIR-TO-AIR MISSILES. THE PROPOSED RESEARCH WILL INVESTIGATE NONLINEAR DECOUPLING AND BIFURCATION ANALYSIS METHODOLOGIES FOR MISSILE AUTOPILOT DESIGN. THE PRIMARY EMPHASIS WILL BE ON BASIC RESEARCH SINCE THE FIELD OF NONLINEAR CONTROL DESIGN IS STILL AT AN EMBRYONIC STAGE.

Principal Investigator:

Donald e gustafson
6176616364

Business Contact:

Small Business Information at Submission:

Scientific Systems Inc
35 Cambridge Park Dr - One Ale Cambridge, MA 02140

EIN/Tax ID:
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No