[go: up one dir, main page]

Ben-Asher et al., 1997 - Google Patents

Optimal guidance with reduced sensitivity to time-to-go estimation errors

Ben-Asher et al., 1997

Document ID
528585880335640307
Author
Ben-Asher J
Yaesh I
Publication year
Publication venue
Journal of Guidance, Control, and Dynamics

External Links

Snippet

The feedback gains can now follow from the inversion of S and the use of Eq.(10). Because of the complexity of the results, this stage is better carried out with numerical values than with symbols. For the interesting special case where a! 1, b D c! 0 (ie, game-theoretic perfect …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • 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
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • 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
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • 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
    • 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
    • G05D1/02Control of position or course in two dimensions
    • G05D1/021Control of position or course in two dimensions specially adapted to land vehicles
    • G05D1/0287Control of position or course in two dimensions specially adapted to land vehicles involving a plurality of land vehicles, e.g. fleet or convoy travelling
    • G05D1/0291Fleet control
    • G05D1/0295Fleet control by at least one leading vehicle of the fleet

Similar Documents

Publication Publication Date Title
Ben-Asher et al. Optimal guidance with reduced sensitivity to time-to-go estimation errors
Lu Augmented apollo powered descent guidance
Shima et al. Time-varying linear pursuit-evasion game models with bounded controls
US6064332A (en) Proportional Guidance (PROGUIDE) and Augmented Proportional Guidance (Augmented PROGUIDE)
Tillerson et al. Distributed coordination and control of formation flying spacecraft.
Williams et al. Modern control theory for design of autopilots for bank-to-turn missiles
Ebrahimi et al. Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers
Williams et al. Design of an integrated strapdown guidance and control system for a tactical missile
Calise Singular perturbation methods for variational problems in aircraft flight
Brunner et al. Comparison of fully numerical predictor-corrector and Apollo skip entry guidance algorithms
Erdos et al. L1 adaptive control integrated missile autopilot and guidance
Yanushevsky et al. New approach to guidance law design
Breitner et al. Complex differential games of pursuit-evasion type with state constraints, part 2: Numerical computation of optimal open-loop strategies
Funk Optimal-path precision terrain-following system
Kim et al. Receding horizon guidance laws with no information on the time-to-go
Hess et al. Preview control pilot model for near-earth maneuvering helicopter flight
Yueh et al. Guidance performance analysis with in-flight radome error calibration
Lee et al. Capture region of tactical missile equipped with semi-active laser seeker using tobit kalman filter
Brunner et al. Comparison of numerical predictor-corrector and Apollo skip entry guidance algorithms
Levinson et al. Trajectory shaping and terminal guidance using linear quadratic differential games
Lorenz et al. A decoupled approach for trajectory generation for an unmanned rotorcraft
Sankar et al. Higher order sliding mode-based guidance for controlling statically unstable missiles
Creaser et al. Fuzzy missile guidance laws
Fan et al. Control of static unstable airframes
Karthikeyan et al. Near Optimal Explicit Guidance Law with Impact Angle Constraints for a Hypersonic Re-entry Vehicle.