[go: up one dir, main page]

Karami et al., 2009 - Google Patents

Spacecraft momentum dumping using fewer than three external control torques

Karami et al., 2009

Document ID
10073924135935614181
Author
Karami M
Sassani F
Publication year
Publication venue
Journal of guidance, control, and dynamics

External Links

Snippet

THRUSTERS perform a key role in spacecraft momentum-dumping procedures. Any external torque, including disturbance torques, changes the overall angular momentum of the spacecraft. Momentum wheels (MWs) apply internal torques to the body of the …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • 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
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • 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
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
    • 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
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1014—Navigation satellites

Similar Documents

Publication Publication Date Title
Wie Solar sail attitude control and dynamics, part two
Kristiansen et al. Satellite attitude control by quaternion-based backstepping
Yoon et al. Spacecraft adaptive attitude and power tracking with variable speed control moment gyroscopes
Tsiotras et al. Satellite attitude control and power tracking with energy/momentum wheels
Horri et al. Practical implementation of attitude-control algorithms for an underactuated satellite
Kang et al. Analytical and experimental investigation of stabilizing rotating uncooperative target by tethered space tug
Hogan et al. Three-axis attitude control using redundant reaction wheels with continuous momentum dumping
CN106933241B (en) Single-gimbal control momentum gyro spacecraft fault tolerant control method based on fault de couple
CN102923317B (en) Under-actuated control method suitable for damping angular velocity of satellite attitude
Ousaloo Globally asymptotic three-axis attitude control for a two-wheeled small satellite
Kojima Backstepping-based steering control for spacecraft attitude control using two-skewed control moment gyroscopes
Junjie et al. Dynamics and de-spin control of massive target by single tethered space tug
CN111897352B (en) Attitude Maneuvering Dynamic Optimization Method and Medium Based on Control Torque Output Constraints
Kojima et al. Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment
Sun et al. Spacecraft formation control using aerodynamic and Lorentz force
Karami et al. Spacecraft momentum dumping using fewer than three external control torques
Maghami et al. Drag-free performance of the ST7 disturbance reduction system flight experiment on the LISA pathfinder
Yoon Spacecraft attitude and power control using variable speed control moment gyros
Yu et al. Torque distribution of the integrated magnetically suspended inertia actuator for attitude maneuvers
Jia et al. Trajectory planning for a space robot actuated by control moment gyroscopes
Barman et al. Satellite attitude control using double-gimbal variable-speed control moment gyroscope: Single-loop control formulation
Reijneveld et al. Attitude control system of the Delfi-n3Xt satellite
Oh et al. Near-eigenaxis rotation control law design for moving-to-rest maneuver
Bedrossian et al. International space station US GN&C attitute hold controller design for orbiter repair maneuver
Steyn A dual-wheel multi-mode spacecraft actuator for near-minimum-time large angle slew maneuvers