Apparatus for compensating a ballistic missile for atmospheric p

Details Apparatus for compensating a ballistic missile for atmospheric p Apparatus for compensating a ballistic missile for atmospheric p

1966-10-10

1978-09-05

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244 315, 244 32, F42B 1512

Patent

active

041113829

ABSTRACT:
A ballistic missile guidance apparatus for compensating the trajectory of a allistic missile just prior to thrust termination by comparing the nominal trajectory with the actual flight parameters encountered during the powered stage of the flight and introducing compensating corrections to provide for an accurate ballistic flight. The comparison is made by storing the nominal kinematic parameters and comparing thereto the actual flight parameters obtained from the inertial guidance system.

REFERENCES:
patent: 2932467 (1960-04-01), Scorgie
patent: 3008668 (1961-11-01), Darlington
patent: 3179355 (1965-04-01), Pickering et al.
patent: 3188019 (1965-06-01), Boutin
patent: 3188958 (1965-06-01), Burke et al.

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