Saleem et al., 2016 - Google Patents

Lyapunov-based guidance law for impact time control and simultaneous arrival

Saleem et al., 2016

Document ID
6167793775692518359
Author
Saleem A
Ratnoo A
Publication year
Publication venue
Journal of Guidance, Control, and Dynamics

External Links

Snippet

INTERCEPTOR guidance laws are designed to satisfy the primary requirement of driving to zero the closing distance to the target. However, many practical engagements impose additional constraints like minimum control effort [1], a desired impact angle [2–5], or a …
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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
    • F41G7/22—Homing guidance systems
    • F41G7/226—Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles

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