NDLI: Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurements

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Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,

Aerospace Control Systems

Index of authors and Chairpersons

Simulation of Missiles and Targets in a Model Ship Level Systems Engineering

An Exact Determination of the Probability Density Function Under Coordinate Transformations

A Computer Algorithm to Estimate Stability Regions Iind to Place Bounds on Settling Times for Nonlinear Systems

Nonlinear Least Squares Estimation in Naval Gun Fire Control

Stability, Aim Bias Compensation and Noise Sensitivity of Phalanx Ciws Control System

High Resolution Harmonic Retrieval Using Jdef (joint Detection/estimation Filter)

High Resolution Target Range Estimation in the Presence of Multipath Using JDEF

Survey of Neural Network Techniques and Relevant Applications

Improved Performance Adaptive Control Under Standard Mrac Assumptions

Constrained Optimal Estimation: An Application to Target State Estimation in the Presence of Multipath Noise

Neural Network Vibration Control Based on Output Feedback

An Adaptive Lattice Filter Approach to Structural, Failure Detection and Localization Based on Acoustic Reflections

Adaptive Control of an Alignment System with Nonlinear Plant Characteristics

Optimal Design of Distributed Sensors and Actuators Made of Smart Materials for Active Vibration Control

Dynamics and Shape Control of Adaptive Structures

Robust Stabilization of the Space Station in the Presence Matrix Uncertainty

Adaptive Friction Compensation Applied to Positioning of a Space-Station Solar Array

Robust Fuel- and Time-Optimal Control of Uncertain Flexible Space Structures

Robust Flexible Spacecraft Control System Design

Robust Controller Design and Mechaneza Tion for Precision Platform Alignment of the Trident II Inertial Measurement Unit (IMU)

Line of Sight Differentiation via Kalman Filter

Functional Analysis of a Passive Sensor Suite ATR/q System

Investigation of Imm Tracking Algorithm for the Maneuvering Target Tracking

Multisensory Data Fusion for Target

Adaptive Traffic Signal Control Using Fuzzy Logic

A method for fuzzy rules extraction directly from numerical data

A New Approach to Sparse Matrix Eigenvalues

Wavelets and operators in the Clifford algebra framework

Some PDE Problems from Estimation Algebras

Some Remarks on Wavelet Transforms

Detection of Signals in 1/f Noise Using Wavelets

Modeling Analog Sun Sensor Current Output

Worst Case analysis for a Precision Clock and Crystal Oscillator Using l/sup 1/ Techniques

Dynamic Modelling of Thermal Shock

Adaptive Robustification of Uncertain Control Systems

Nonlinear Flight Control Using Neural Networks and Feedback Linearization

A Distributed Parameter System Model for Active Control of a Large, Flexible Phased Array Transmitter

Control for Unstable Non-Minimum Phase Uncertain Dynamic Vehicle

Design of Dynamic Compensators for Linear Parameter-Varying Feedback Systems by the Gain Scheduling Technique

Performance Analysis for Recursive Passive Adaptive Controllers

A parallel adaptive neural network control system, with application to real-time control of a servomechanism with asymmetrical loading

Interpretations of Digital Controller for Process Control System

Hybrid Optimal Control of Large-Scale Linear Systems

Advanced Instrumentation for Next Generation Aerospace Propulsion Control Systems

"Total" Current Control of Brushless DC Motors with Sinewave Drive

Stability Robustness Against Real Parameter Uncertainty of DC Electrical Power Conversion Systems

Throttle Control for Vehicle Following

Adaptive Tracking Control for a DC Motor

On Control Design for a Fluid-Structure Interaction Problem

Inverter Gain Compensation for Open Loop and Current Regulated Pwm Controllers

Fuzzy Variable Structure Controller for Chattering Reduction

Evaluation of Classical and Fuzzy Logic Controllers for Wind Turbine Yaw Control

Neural Intelligent Control for Maneuvering Spacecraft

Adaptive Neural Network Control of a Helicopter in Vertical Flight

Intelligent Self-Tuning Control of Varying Delay Systems

A neural-network controller for highly-coupled complex mechanical systems

The Application of Intelligent Control System in a Power Plant

Maximum Allowable Gain Calculation for Guaranteed Performance of Uncertain Systems

Stabilization with Saturated Actuators, a Worked Example: F-8 Longitudinal Flight Control

Self-Organizing Controllers for High Performance Helicopters

Design of a Helicopter Control System to Meet Handling Quality Specifications Using H/spl infin/ Techniques

Robust Control Law for Advanced Flight Control System

Sliding Mode Control Design for Aircraft Control Systems

OptiImal l/sup 1/ Estimation

Application of Robust Game Theoretic Synthesis to the Benchmark Problem

Robust Controller Design for the Benchmark Problem Using the Q-Parameterization Theory

Control of Parameter-Dependent Systems: Applications to H/sub /spl infin/ Gain-Scheduling

The Largest Robust Staeklity Radius, Approximation and Model Reduction

An l/sub /spl infin/ Solution for Approximate Feedback Linearization

A Survey of Experiments for Modeling Verification and Control of Flexible Robotic Manipulators

Transient Dynamic Analysis of Rotating Beams Using Second-Order Theory: A Finite Difference Approach

Minimum-Time Control for Multiple Manipulator Systems

ERA Identification for a Two-link Flexible Manipulator

Transient Dynamics of Rotating Flexible Structures-ModeIing

Transient Dynamics of Rotating Flexible Structures-Simulation

Nonlinear Control of Unbalanced Gimbal Mechanisms

Application of H-Infinity Technique

Real-Time Attitude Estimation Bias Correction for Scanning Surveillance Sensors

Stirling-Cycle Cryocooler Active Vibration Control

A Survey of Simplicial Algorithms and Topology in Robust Stability

Robust Stability and Game of Hex

H/sub /spl infin// Optimal Control of a Simple Nonlinear System Analyzed using Simplicial Algorithms

Simplicial Stability Analysis of an Unstable Plant with Adaptive Perturbation Control

Global Optimization in Control Systems Analysis

Coverage Modelling for Reliability Assessment Self-Repairing Flight Control Systems

Nonlinear Adaptive Control of High Performance Aircraft Using Neural Networks

Genetic Design of Multivariable Flight-Control Systems Using Eigenstructure Assignment

Longitudinal Control of Hypersonic Aircraft: an Alpha Follow-Up Scheme

On the Control of a Simplified Rocking Delta Wing Model

Mimo Environmental Control for Fighter Cockpits

Lateral-Directional Control for High Angle of Attack

Robust Fixed Order Dynamic Compensation: a Differential Game Approach

Aircraft Model Comparison For Minimum Time-To-Climb Problem

2-D and 3-D Minimum-Time-to-Turn Flights by Parameter Optimization

Optimal Evasive Aircraft Maneuvers Against a Surface-To-Air Missile

A Better Trajectory for Approximately Feedback Linearized Systems

On Local Feedback Stabilization of Nonlinear Systems in Critical Cases

Constraining the Motion of a Robot Manipulator Using the Vector Potential Approach

Active Stabilization of Rotating Stall in Axial-Flow Gas Compressors

On the Achievable Performance of a State Feedback Nonlinear H/sub /spl inifin// Control

Solvability Conditions for the General Nonlinear Servomechanism Problem

Modelling of Quantum Control and Inverse Problem

Dealing with the Constraints in Multibody Systems Dynamics

Robust H/spl infin/ Controller Design of Two-link Robots

A robust Sliding Mode Control Scheme for Robotic Manipulators

Classification of Underwater Targets with Active Sonar

Comparative Study of Self-Organizing Neural Networks in Signal Detection and Classification

Joint Detection/Estimation Filter with Application to Image Fusion

Target Detection and Localization from Bearing-Only and Bearing/range Measurements

High Resolution Model Order Selection and Parameter Estimation Using JDEF (Joint Detection/Estimation Filter)

Seeker-Optimized Guidance Integrated Fuzing

/spl mu/-Synthesis Robust Control: What's wrong and how to fix it?

Application of Sliding Mode Control to Bank-To-Turn Missile Systems

Wing Missiles Stabilization Based on Sliding Mode Control

Discrete Advanced Guidance for High Order Acceleration Constrained Missile and Maneuvering Target

Disturbance Attenuation for Guidance and Control

Dual Control Guidance Law for Homing Missiles

Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurements

Design of a Robust Multi-Radar Distributed Data Fusion System

Adaptive Classification for Automatic Target Recognition

High Resolution Multi-Radar Data Fusion Using JDEF

Discrete-Time Mode Filters for Markovian Jump Processes

Multisensory Fusion Algorithms for Tracking

"On the- Filtering of Linear Stochastic Systems with Jumping Coefficients"

Low-order Controller Design of Linear Multivariable Systems Via a Classical Approach

On global stability of quadratic state feedback controlled linear systems

Optimal Eigenvalue Placement Linear Quadratic Performance

Quadratic Lyapunov Functions for Orbitally-Stable Systems

State Feedback Nonlinear H/spl infin/m Control with Guaranteed Region of Performance

Direct Design of Handling Qualities by "Mu - Synthesis"

Optimum Architectures for Multiresolutional Control

Nested Motion Planning for an Autonomous Robot

Control of Stochastic Linear Uncertain Systems by Multiple Objective Optimization

A Distributed Expert System for Stability Analysis

Hierarchical Heuristic Control with Artificial Neural Network for Modelling and Compensation

Advanced Laboratory Equipment In Control Education

A Unique Model of Switching Converters for SPICE

Computational Techniques Based on the Block-Diagonal Form for Solving Large Systems Modeling Problems

Systematic Procedures for the H/spl infin/ Controller Design of a Single Flexible Link

A Generic Controller

Adaptive Attitude Control

Missile Autopilot Design Using a Generalized Hamiltonian Formulation

Designing Autopilot by Nonlinear Servomechanism Theory

Design of Guidance Law for Homing Missile Via Feedback Linearization

Guidance to Collision of a Variable-Speed Missile

Application of Mixed Strategies for Improved Missile - Guidance Nondimensional Sensitivity Analysis

A Constrained Pole Placement Method for Autopilot Gain Scheduling

Autopilot Design Using the Parameter Space and QFT Methods

Transfer Alignment Design and Evaluation Environment

Rapid and Robust Transfer Alignment

Gravity Observation Based Alignment Transfer

GPS Navigation Requirements for Future Mobile Ground-Based Missile Systems

Performance Needs for Advanced Kinetic Energy Missiles' Inertial Measurement Units

Application of GPS for Missile Post Flight Guidance Accuracy Analysis

AC-130U Aircraft Gps-INS Integration

Stable State-Space System Identification from Frequency Domain Data

Initial Investigation of Modal Parameter Estimation for Flexible Manipulator Using Hopfield Network

Robust Control of Flexible Structures Using Multiple Shape Memory Alloy Actuators

Robust Adaptive Control and its Application to a Mechanical Manipulator

Extended Kalman Filter and Neural Network Filter: Who Outperforms Whom in System identification?

Adaptive Estimation of a Flexible Beam

Variable Structure State and Input Observation

Analog VLSI Neural Network Testing

Automated and Objective System Identification Based on Canonical Variables

Identification and filtering of nonlinear systems using canonical variate analysis

Identification and Model Reduction of the ASTREX structure

State Observability and Parameters Identifiability of Stochastic Linear Systems

Fuzzy Logic Enhanced Control of Nonlinear Flexible Pointing Systems

On 'A Tutorial Comparison of Three Multivariable Stability Margins'

Optimality-Based Trajectory Shaping Guidance Design

Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurements

Content Provider	IEEE Xplore Digital Library
Author	Rusnak, I.
Copyright Year	1993
Description	Author affiliation: Drexel University, ECE Dept., Philadelphia, PA (Rusnak, I.)
Abstract	An explicit, closed form formulae of advanced guidance laws for a linear, time-invariant, acceleration-constrained arbitrary-order missile, and a linear, time-invariant, arbitrary-order, randomly maneuvering target with noisy position measurements are derived. Two approaches are presented. The first approach derives the optimal guidance law for a quadratic objective. The solution is the guidance law for deterministic system with limiting on the commanded acceleration applied on the estimated state. The second approach is based on the idea of applying the average of the input that would have been applied to the plant if the noises were known. The formulas of the different guidance laws are given in terms of the transfer function of the missile and acceleration constraint, the shaping filter of the maneuver of the target, responses to initial conditions, error variance matrix of the estimated state and weights in the criterion. It is demonstrated by simulations that although the optimal guidance law has improved performance in terms of the miss distance, the suboptimal average input guidance law consumes less energy.
Starting Page	594
Ending Page	598
File Size	453343
Page Count	5
File Format	PDF
DOI	10.1109/AEROCS.1993.721003
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1993-05-25
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Missiles Technological innovation Stochastic resonance Optimal control Stochastic processes Differential equations Vectors Acceleration Noise measurement State estimation
Content Type	Text
Resource Type	Article

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