Open AccessBook
Tactical and strategic missile guidance
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
Adaptive, Integrated Guidance and Control for Missile Interceptors
Manu Sharma,Nathan D. Richards +1 more
TL;DR: In this paper, an adaptive, integrated guidance and control approach for ballisticmissile interceptors using backstepping control techniques is presented, which is restricted to the pitch-plane, but can be readily extended to all three axes.
Journal ArticleDOI
Proportional navigation guidance using predictive and time delay control
TL;DR: In this article, a new formulation of the proportional navigation guidance law using the continuous time nonlinear predictive control approach is proposed to estimate the target acceleration using the time delay control (TDC).
Journal ArticleDOI
Autonomous navigation for the deep impact mission encounter with comet tempel 1
TL;DR: In this paper, the authors describe the Impactor s/c autonomous targeting design and the Flyby s /c autonomous tracking design, including image processing and navigation (trajectory estimation and maneuver computation), and discuss the analysis that led to the current design, the expected system performance as compared to the key mission requirements and the sensitivity to various s/C subsystems and Tempel 1 environmental factors.
Journal ArticleDOI
Time-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement
TL;DR: A new impact angle control guidance law is introduced for a homing missile system equipped with a passive seeker against a stationary or slowly moving target that provides sufficient trajectory modulations, such as oscillatory trajectories, to enhance target observability from angle-only measurements.
Proceedings ArticleDOI
Cooperative aircraft defense from an attacking missile
TL;DR: This paper addresses a three-body pursuit-evasion scenario where an Attacker missile using Pure Pursuit guidance pursues a Target aircraft and a Defender missile launched by a wingman aims at intercepting the Attacker before it reaches the aircraft.