ADAPTIVE AUTOPILOT
Assignee
Filed
Jun 20, 1974
Granted
Sep 28, 1993
Location
CA US
Abstract
An autopilot system including parameter identification circuits wherein the function of the torque and the function of the translational force on a missile are unknown and varying (including approaching zero).
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 1, 1982
Rescinded
Apr 10, 1991
Duration
8 years, 6 months
Inventor
- 1DEWEY P. ANKENEY
Record Details
- Patent number
- US 5248114
- Application
- 00548157
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
More from this assignee
IMPROVED CATALITIC SYNTHESIS OF CAGED POLYNITRAMINE COMPOUNDS
SOLID ROCKET PROPELLANT
DUAL INFRARED BAND OBJECTIVE LENS
BANDGAP RADIATION DETECTOR
METHOD OF FORMING TEXTURED HIGH-TEMPERATURE SUPERCONDUCTORS
APPARATUS FOR CONTROLLING THE POSITION AND DIRECTION OF A LASER BEAM
Related by domain
IMPROVED PERFORMANCE EXLPOSIVE-FORMED PROJECTILE
GIAT INDUSTRIES
MULTIPLE INFRARED MISSILE JAMMER
LOCKHEED SANDERS INC, A DELAWARE CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
MISSILE LAUNCHER
MBM TECHNOLOGY LIMITED
AIR TO AIR HOMING MISSILE GUIDANCE
AIR FORCE, UNITED STATES OF AMERICA, AS REPRESENTED BY, THE SECRETARY
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION