DocumentCode
343956
Title
Control architecture for increased performance in pointing lasers
Author
Cusumano, Salvatore ; Robertson, Laweuce ; Tellez, Lt Jason ; Tipton, Charly ; Jordan, David ; Ratte, Keith
Author_Institution
ABL Technol., Kirtland AFB, NM, USA
Volume
3
fYear
1999
fDate
1999
Firstpage
351
Abstract
An overview of a control´s architecture for pointing a laser in a track loop that performs with low frequency, type II, error rejection without the use of two free integrators in the forward path is presented. The method uses a stabilization loop on the outgoing laser to follow the residual error of the track loop. The cost of this loop is the addition of a position sensor and correction mirror. These components are normally used in high-performance pointing systems, thus the cost is only the delta increase in requirements from a conventional loop to that proposed. Additional effort is needed to calibrate the track sensor and stabilization sensor such that errors can be cross referenced. This capability allows for the additional error rejection between the two loops. The ability to accurately calibrate these detectors limits the performance of the total loop interaction. Initial simulation results show excellent type II error rejection without the overshoot typical in classical type II error rejection loops
Keywords
digital simulation; error correction; laser beam applications; military computing; missile control; optical tracking; pointing systems; real-time systems; GUI; additional error rejection; calibration; control architecture; correction mirror; pointing lasers; position sensor; real time system; residual error; simulation; stabilization loop; stabilization sensor; track loop; type II error rejection; Costs; Error correction; Force control; Mirrors; Missiles; Optical control; Optical sensors; Power engineering and energy; Target tracking; Tracking loops;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location
Snowmass at Aspen, CO
Print_ISBN
0-7803-5425-7
Type
conf
DOI
10.1109/AERO.1999.789795
Filename
789795
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