Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1974-11-21
1976-08-31
Wilbur, Maynard R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
250203R, 356 4, 356152, F41G 700
Patent
active
039776280
ABSTRACT:
A tracking and/or guidance system is disclosed for defining a route to be followed by a vehicle or projectile to a target. The system includes a tracking device which is arranged firstly to operate in an acquisition mode, applicable when the vehicle or projectile is close to the device, and subsequently to be progressively converted into a tracking mode as the distance between the vehicle or projectile and the device increases. In the acquisition mode, the device has a wide field of view but is relatively insensitive to deviations of said vehicle or projectile from said route. As the aforesaid distance increases, however, the field of view is progressively reduced and the sensitivity to said deviations is progressively increased. The invention thus provides a system which is suitable for the both initial acquisition and long range guidance of a vehicle or projectile aimed towards a distant target whilst using a conveniently small detector arrangement.
REFERENCES:
patent: 3218909 (1965-11-01), Fain
patent: 3296443 (1967-01-01), Argyle
patent: 3497695 (1970-02-01), Smith
patent: 3638025 (1972-01-01), Dishington
Buczinski S. C.
EMI Limited
Wilbur Maynard R.
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