Missile Guidance and Control System Design Trends

Format:

Conference/Event

Author/Creator:

George, Leo C., author.

Conference Name:

Aerospace Engineering and Manufacturing Meeting (1974-09-30 : San Diego, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1974

Summary:

This paper describes selected guidance and control (G and C) concepts that are currently being considered for use on one or more advanced missile systems and, in the opinion of the author, represent trends in missile G and C system design. The guidance system concept to be described is the floated inertial measurement ball (FLIMBAL), and the control system concept is based on the single movable nozzle design configuration.In addition, a description of selected design trends applicable to both guidance and control system hardware is presented which includes inertial instruments, electronics design, nuclear hardness considerations, and data transmission techniques

Notes:

Vendor supplied data

Publisher Number:

740873

Access Restriction:

Restricted for use by site license