[go: up one dir, main page]

Burchett et al., 2002 - Google Patents

Model predictive lateral pulse jet control of an atmospheric rocket

Burchett et al., 2002

Document ID
12532511194684986010
Author
Burchett B
Costello M
Publication year
Publication venue
Journal of Guidance, Control, and Dynamics

External Links

Snippet

DIRECT fi re atmospheric rockets are fi red by line-of-sightaiming and are fi red from ground- based platforms, helicopters, and fi xed-wing aircraft. These rockets exit the launcher with low speed. Any aerodynamic disturbances presented to the rocket near the launcher create …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/24—Beam riding guidance systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming means; Laying means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/12—Target-seeking control

Similar Documents

Publication Publication Date Title
Burchett et al. Model predictive lateral pulse jet control of an atmospheric rocket
Kim et al. Look-angle-shaping guidance law for impact angle and time control with field-of-view constraint
Pastrick et al. Guidance laws for short-range tactical missiles
Jitpraphai et al. Dispersion reduction of a direct fire rocket using lateral pulse jets
Ohlmeyer et al. Generalized vector explicit guidance
Dukeman Atmospheric ascent guidance for rocket-powered launch vehicles
Özkan Dynamic modeling, guidance, and control of homing missiles
Pavkovic et al. Frequency-modulated pulse-jet control of an artillery rocket
Lukacs et al. Trajectory-shape-varying missile guidance for interception of ballistic missiles during the boost phase
Yang Impact-point-based guidance of a spinning artillery rocket using canard cyclic control
Phillips Guidance algorithm for range maximization and time-of-flight control of a guided projectile
Wan et al. Suboptimal Midcourse Guidance with Terminal‐Angle Constraint for Hypersonic Target Interception
Gnemmi et al. Flight phases with tests of a projectile-drone hybrid system
Calise An analysis of aerodynamic control for direct fire spinning projectiles
US5875993A (en) Flight control of an airborne vehicle at low velocity
Braun et al. Advances in inertial guidance technology for aerospace systems
Khamis et al. Nonlinear Finite‐Horizon Regulation and Tracking for Systems with Incomplete State Information Using Differential State Dependent Riccati Equation
Sreeja et al. Precision munition guidance and moving-target estimation
Pavic et al. Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism
Mathavaraj et al. Optimally allocated nonlinear robust control of a reusable launch vehicle during re-entry
Blakelock Design and analysis of a digitally controlled integrated flight/firecontrol system
Gaudet et al. A comparison of partially and fully integrated guidance and flight control optimized with reinforcement meta-learning
Fresconi et al. Delivery of modular lethality via a parent-child concept
Nobahari et al. Integrated optimization of guidance and control parameters in a dual spin flying vehicle
Kim et al. Guidance and control system design for impact angle control of guided bombs