Kim et al., 2013 - Google Patents

Bias-shaping method for biased proportional navigation with terminal-angle constraint

Kim et al., 2013

Document ID
3159150534806590748
Author
Kim T
Park B
Tahk M
Publication year
Publication venue
Journal of Guidance, Control, and Dynamics

External Links

Snippet

FOR decades, many advanced guidance laws with terminal-impact-angle constraints have been devised to maximize the warhead effect of antiship or antitank missiles and to ensure a high kill probability. The proposed suboptimal guidance with a terminal body-attitude …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2293Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/226Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements

Similar Documents

Publication Publication Date Title
Kim et al. Bias-shaping method for biased proportional navigation with terminal-angle constraint
Cho et al. Nonsingular sliding mode guidance for impact time control
Erer et al. Indirect impact-angle-control against stationary targets using biased pure proportional navigation
Ratnoo et al. Impact angle constrained interception of stationary targets
Lee et al. Interception angle control guidance using proportional navigation with error feedback
He et al. Optimality of error dynamics in missile guidance problems
Hu et al. New impact time and angle guidance strategy via virtual target approach
Kumar et al. Nonsingular terminal sliding mode guidance with impact angle constraints
Kumar et al. Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints
Ratnoo et al. Impact angle constrained guidance against nonstationary nonmaneuvering targets
Tekin et al. Switched-gain guidance for impact angle control under physical constraints
Cho et al. Optimal impact angle control guidance law based on linearization about collision triangle
Shaferman et al. Linear quadratic guidance laws for imposing a terminal intercept angle
Park et al. Composite guidance scheme for impact angle control against a nonmaneuvering moving target
Tekin et al. Polynomial shaping of the look angle for impact-time control
Saleem et al. Lyapunov-based guidance law for impact time control and simultaneous arrival
Shaferman et al. Cooperative optimal guidance laws for imposing a relative intercept angle
Liu et al. Closed-loop optimization of guidance gain for constrained impact
Lu et al. Adaptive terminal guidance for hypervelocity impact in specified direction
Ratnoo Analysis of two-stage proportional navigation with heading constraints
Tsalik et al. Circular impact-time guidance
Zhou et al. Guidance laws with finite time convergence
Cottrell Optimal intercept guidance for short-range tactical missiles
Dhananjay et al. Accurate time-to-go estimation for proportional navigation guidance
Zhou et al. Adaptive dynamic surface guidance law with input saturation constraint and autopilot dynamics