Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1973-08-10
1984-03-27
Walsh, Donald P.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 1502
Patent
active
044388934
ABSTRACT:
In a projectile including a spinning main housing and a despun canard frame having deflectable canards thereon, a pair of stator windings are disposed within the main housing and a cooperating pair of rotors are arranged within the canard frame. The first stator windings and corresponding rotor generate prime power and permit control of the rotational position of the canard frame while the second stator windings and associated rotor allow control of the deflectable canards.
REFERENCES:
patent: 2920568 (1960-01-01), Rabinow
patent: 2990776 (1961-07-01), Clarke
patent: 3067681 (1962-12-01), Beman
patent: 3111088 (1963-11-01), Fisk
patent: 3125027 (1964-03-01), Stoller
Sands Timothy B.
Sinclair Ronald R.
Etlinger Louis
Ryan Maureen T.
Sanders Associates Inc.
Seligman Richard I.
Walsh Donald P.
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