Integrated Strapdown Avionics for Precision Guided Weapons

Conventional avionic configurations for precision guided weapons are often unnecessarily costly and inefficient because of built-in (but unused) redundancy in instrumentation attributed to the present day independent systems design approach. Described in this paper is an integrated design approach using strapdown avionic components that has the potential for lowering cost, increasing realibility and improving overall performance as a result of using fewer and less costly instruments in an optimum manner.

[1]  Bernard Friedland,et al.  Design of an integrated strapdown guidance and control system for a tactical missile , 1983 .

[2]  T. Bullock,et al.  Maneuver detection and tracking with a nonlinear target model , 1984, The 23rd IEEE Conference on Decision and Control.

[3]  Bernard Friedland,et al.  Maximum likelihood estimation of target acceleration , 1984, The 23rd IEEE Conference on Decision and Control.