scispace - formally typeset
Open AccessBook

Tactical and strategic missile guidance

Paul Zarchan
Reads0
Chats0
TLDR
In this paper, a three-loop Autopilot is used to provide tactical and strategic guidance for a single-antenna MIMO-BMG system using MATLAB units.
Abstract
Numerical Techniques Fundamentals of Tactical Missile Guidance Method of Adjoints and the Homing Loop Noise Analysis Convariance Analysis and the Homing Loop Proportional Navigation and Miss Distance Digital Fading Memory Noise Filters in the Homing Loop Advanced Guidance Laws Kalman Filters and the Homing Loop Other Forms of Tactical Guidance Tactical Zones Strategic Considerations Boosters Lambert Guidance Strategic Intercepts Miscellaneous Topics Ballistic Target Properties Extended Kalman Filtering and Ballistic Coefficient Estimation Ballistic Target Challenges Multiple Targets Weaving Targets Representing Missile Airframe with Transfer Functions Introduction to Flight Control Design Three-Loop Autopilot. Appendices: Tactical and Strategic Missile Guidance Software Converting Programmes to C Converting Programmes to MATLAB Units.

read more

Citations
More filters
Proceedings ArticleDOI

Guidance law for formation flight via desired position

TL;DR: In this paper, a leader-follower concept is proposed for formation flight control, where the desired positions for followers are derived using only the leader's position information and the well-known PNG law is selected to guide the follower to the desired position.
Proceedings ArticleDOI

Sliding mode based attitude and acceleration controller for a velocity-varying skid-to-turn missile

TL;DR: In this article, a sliding mode based roll-pitch-yaw integrated attitude and acceleration controller for a fin-controlled skid-to-turn (STT) missile is proposed.
Proceedings ArticleDOI

Integrated missile flight control using quaternions and Third-order sliding mode control

TL;DR: 6-Degree of Freedom simulations of a simplified missile model with and without realistic actuator models, delays and parametric uncertainties confirms the efficacy of the proposed robust integrated HOSM guidance/control design.
Proceedings ArticleDOI

A high-order sliding mode variable structure guidance law with finite time convergence

TL;DR: The paper proposes a robust guidance law with high-order sliding mode variable structure to handle the problems of poor convergence and the control chattering variable structure considering limited guidance information when the target is suffering the high maneuver interception.
Journal ArticleDOI

Target Acceleration Estimation from Radar Position Data using Neural Network

TL;DR: In this paper, a preliminary investigation on target manoeuvre estimation in real-time from the available measurements of noisy position data from tracking radar using an artificial neural network (ANN) was conducted.