Abstract A pedestal and gimbal assembly related to missile semi-active radar seekersor supporting three gyroscopes and functions as a reference platform to relate airframe attitude. This is mechanized by utilizing the two degrees of freedom gimbal for pitch and yaw and controlling the missile body roll axis for the third degree of freedom. Structure of the positioning system includes a pedestal having an inner gimbal assembly including a support for mounting the antenna assembly and the gyros. A yaw torque motor assembly is carried by the inner gimbal and is provided with a pair of output shafts for supporting the inner gimbal and controlling the yaw movement thereof. A pitch motor is housed in the pedestal and includes a drive pinion and a drive shaft. The drive pinion is connected to the drive shaft. The drive pinion and yaw motor operates to control the pitch movement of the antenna assembly.
Inventors
👤 Raymond J. Estlick
👤 Oscar E. Swenson
Bibliographic Details
Application Number—
JurisdictionUS
Data Sourcegoogle_patents
Last Synchronized2026-11-05 08:46
CPC Classifications
H; H01; H01Q; H01Q1/00; H01Q1/12; H01Q1/18
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
115 words
In an antenna positioning system, a pedestal and gimbal assembly for supporting components of the system including an antenna assembly and three gyros comprising: a pedestal; an inner gimbal assembly including a support for mounting said antenna assembly and said gyros; a yaw torque motor assembly carried by said inner gimbal and having a pair of hollow output shafts for supporting said inner gimbal and controlling the yaw movement therefor; a pitch motor housed in said pedestal and having a drive pinion and a drive shaft, said drive pinion connected to said drive shaft; and, means connected between said drive pinion and said yaw motor assembly for controlling the pitch movement of said antenna assembly.
Claim 2
Dependent Claim
115 words
In an antenna positioning system, a pedestal and gimbal assembly for supporting components of the system including an antenna assembly and three gyros comprising: a pedestal; an inner gimbal assembly including a support for mounting said antenna assembly and said gyros; a yaw torque motor assembly carried by said inner gimbal and having a pair of hollow output shafts for supporting said inner gimbal and controlling the yaw movement therefor; a pitch motor housed in said pedestal and having a drive pinion and a drive shaft, said drive pinion connected to said drive shaft; and, means connected between said drive pinion and said yaw motor assembly for controlling the pitch movement of said antenna assembly.
Claim 3
Dependent Claim
41 words
An assembly as set forth in claim 1 wherein said yaw torque motor assembly includes a cast housing and a pair of motor stator bush riggings attached to said cast housing and adjustable preloaded ball bearings for supporting said output shafts.
Claim 4
Dependent Claim
41 words
An assembly as set forth in claim 2 wherein said cast housing is provided with a pitch shaft perpendicular to the yaw axis and bearing to support the pitch shaft, said pitch shaft and said yaw motor output shafts being hollow.
Claim 5
Dependent Claim
24 words
An assembly as set forth in claim 3 wherein said cast housing is further provided with a weight for pitch balancing of said housing.
Claim 6
Dependent Claim
42 words
An assembly as set forth in claim 4 wherein said pedestal is provided with a pitch potentiometer having an anti-backlash gear attached to its output shaft, said pitch motor drive shaft having a second drive pinion for engagement with said anti-backlash gear.
Claim 7
Dependent Claim
39 words
An assembly as set forth in claim 5 wherein a pitch sector gear is attached to said cast housing and is connected to the first drive pinion for movement thereby to control the pitch movement of the antenna assembly.