Extraction and Filter Algorithm of Guidance Information for Full-strapdown Seeker on Rotation Missile

Guidance Law Evaluation for Missile Guidance Systems

In missile guidance system, to reduce the interception “miss distance,” it is important to choose a suitable guidance law and navigation constant. This paper investigates and compares the system behavior of guidance laws under different navigation constants. Based on use of the adjoint technique, miss distance sensitivity analyses which consider the system noise, target step maneuver, initial h...

New Principle for Missile Guidance and Control

ted to allow efficient ballistic missiles , the paper describes a recently developed ted estimation/guidance design paradigm n several innovative concepts that provides satisfactory homing performance against ly maneuvering targets. The new paradigm veloped and tested first by using a simplified constant speed interception scenario model. paper the integrated estimation/guidance m is validated ...

Missile Guidance and Control Systems

Robot Arm Trajectory Planning Using Missile Guidance Algorithm

This paper presents a novel approach to on-line trajectory planning of robot arms for the interception of a fastmaneuvering object under torque and velocity constraints. Especially, the trajectory planning in the Y direction employs a missile guidance algorithm to intercept the maneuvering object. The proposed method yields that a robot arm can smoothly grasp a maneuvering object. Simulation re...

Optical Performance Anal Ysis of Standard Missile Blockiy a Seeker

The flight environment of the Standard Missile, Block IV A interceptor involves high speeds that place severe aerodynamic and aero-thermalloads on the missile optical window and sensor. The supersonic flow over the missile produces aero-optical effects that can degrade IR seeker performance. This report summarizes an analysis of aero-optical aberrations due to shock front and shear layer densit...