[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Liu et al., 2016 - Google Patents

Predictor-corrector guidance for entry with terminal altitude constraint

Liu et al., 2016

View PDF
Document ID
237733740231684670
Author
Liu S
Liang Z
Li Q
Ren Z
Publication year
Publication venue
2016 35th Chinese Control Conference (CCC)

External Links

Snippet

A novel predictor-corrector guidance algorithm is presented for the entry flight with the terminal altitude constraint. Previous predictor-corrector algorithms focus mainly on the flight range control, thus the terminal altitude error is large in dispersed cases. To improve the …
Continue reading at www.researchgate.net (PDF) (other versions)

Classifications

    • 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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/042—Control of altitude or depth specially adapted for aircraft
    • G05D1/046—Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants

Similar Documents

Publication Publication Date Title
Sun et al. Adaptive backstepping control of spacecraft rendezvous and proximity operations with input saturation and full-state constraint
Zhang et al. Entry trajectory planning based on three-dimensional acceleration profile guidance
Yang et al. Autonomous entry guidance using linear pseudospectral model predictive control
Wang et al. A robust predictor–corrector entry guidance
Zhang et al. Entry guidance for high-L/D hypersonic vehicle based on drag-vs-energy profile
Liao-McPherson et al. Model predictive control strategies for constrained soft landing on an asteroid
Sun et al. Saturated adaptive relative motion coordination of docking ports in space close-range rendezvous
Dai et al. Mars atmospheric entry guidance for reference trajectory tracking based on robust nonlinear compound controller
Qi et al. Self-healing control design under actuator fault occurrence on single-rotor unmanned helicopters
Lu Entry guidance using time-scale separation in gliding dynamics
Gong et al. Mars entry guidance for mid-lift-to-drag ratio vehicle with control constraints
Liang et al. Entry guidance with terminal approach angle constraint
Liang et al. Decoupling trajectory tracking for gliding reentry vehicles
Liang et al. Lateral Entry Guidance With Terminal Time Constraint
Liu et al. Predictor-corrector guidance for entry with terminal altitude constraint
Shen et al. Point return orbit design and characteristics analysis for manned lunar mission
Sushnigdha et al. Trajectory design of re-entry vehicles using combined pigeon inspired optimization and orthogonal collocation method
Sushnigdha et al. Evolutionary method based integrated guidance strategy for reentry vehicles
Zhou et al. A simple reentry trajectory generation and tracking scheme for common aero vehicle
Wang et al. Six-DOF trajectory optimization for reusable launch vehicles via Gauss pseudospectral method
Yang et al. Entry guidance with no-fly zone avoidance using linear pseudospectral model predictive control
Lei et al. A steering method with multiobjective optimizing for nonredundant single-gimbal control moment gyro systems
Afshari et al. Determination of nonlinear optimal feedback law for satellite injection problem using neighboring optimal control
Liang et al. Optimal bank reversal for high-lifting reentry vehicles
Wang et al. Entry guidance command generation for hypersonic glide vehicles under threats and multiple constraints