Catalogue Search | MBRL
Search Results Heading
Explore the vast range of titles available.
MBRLSearchResults
-
DisciplineDiscipline
-
Is Peer ReviewedIs Peer Reviewed
-
Item TypeItem Type
-
SubjectSubject
-
YearFrom:-To:
-
More FiltersMore FiltersSourceLanguage
Done
Filters
Reset
2
result(s) for
"vertical-plane maneuvering"
Sort by:
Numerical Investigation of Maneuvering Characteristics for a Submarine Under Horizontal Stern Plane Deflection in Vertical Plane Straight-Line Motion
2025
The maneuverability of a submarine in the vertical plane is a key indicator of navigation safety. However, existing studies typically evaluate maneuvering performance based on hydrodynamic coefficients, often neglecting the flow-field evolution induced by different steering strategies. In this study, a high-fidelity numerical model for the vertical-plane motion of the DARPA SUBOFF submarine is established using the Reynolds-Averaged Navier–Stokes (RANS) method and validated against benchmark data. Unlike traditional analyses that employ a fixed rudder angle, this work systematically compares three steering strategies with continuously varying rudder angles—trapezoidal, step, and linear steering—examining their motion responses, hydrodynamic performance, and unsteady flow-field evolution. The results show that, although step steering produces the fastest response with the strongest transient characteristics, it also triggers pronounced flow separation and significant unsteady effects. Linear steering yields a smoother but the weakest motion response, with reduced rudder effectiveness and a noticeable lag effect. In contrast, trapezoidal steering maintains a stable flow field around the submarine, with uniformly concentrated vorticity distribution, ensuring smooth and safe motion and achieving a favorable balance between response speed and flow stability. The findings provide theoretical reference for research on submarine vertical-plane steering motion, rudder-angle control, and flow-field stability.
Journal Article
Optimal Guidance of Rockets
by
Reynolds, Harry
,
Tewari, Ashish
in
3DPN guidance system ‐ and inertia dynamics, feedforward reference input
,
ballistic missile launch ‐ guiding a gravity‐turn rocket
,
fast response times ‐ in translation and rotation of rockets
2011
This chapter contains sections titled:
Introduction
Optimal Terminal Guidance of Interceptors
Non‐planar Optimal Tracking System for Interceptors: 3DPN
Flight in a Vertical Plane
Optimal Terminal Guidance
Vertical Launch of a Rocket (Goddard's Problem)
Gravity‐Turn Trajectory of Launch Vehicles
Launch of Ballistic Missiles
Planar Tracking Guidance System
Robust and Adaptive Guidance
Guidance with State Feedback
Observer‐Based Guidance of Gravity‐Turn Launch Vehicle
Mass and Atmospheric Drag Modeling
Summary
Exercises
References
Book Chapter