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公开(公告)号：WO2020047383A1
公开(公告)日：2020-03-05
申请号：PCT/US2019/049013
申请日：2019-08-30
Inventor： ZEMANY, Paul D. , CHROBAK, Matthew, F. , DEGTIAREV, Egor V.
Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.
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公开(公告)号：WO2015122955A3
公开(公告)日：2015-08-20
申请号：PCT/US2014/067793
申请日：2014-11-27
Inventor： CHOINIERE, Michael J. , DEGTIAREV, Egor V. , GAUSCH, Eric C. , JANIAK, Derek P.
Abstract: A laser range finder (LRF) and an automated method for determining a return laser signal associated with a target thereof are disclosed. In one example embodiment, the LRF includes a laser beam emitter to emit a laser beam towards a target. Further, the LRF includes a receiver circuit to receive multiple return laser signals reflected from objects including the target and to determine an amplitude of each of the multiple return laser signals. Furthermore, the LRF includes a processor coupled to the receiver circuit to compare the amplitude of each of the multiple return laser signals with a range varying threshold that accounts for range and atmospheric losses and to determine one of the multiple return laser signals as being associated with the target based on the comparison.
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公开(公告)号：EP3631914A1
公开(公告)日：2020-04-08
申请号：EP17910559.8
申请日：2017-05-25
Inventor： CHOINIERE, Michael J. , DEGTIAREV, Egor V.
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