Schaub, 2008 - Google Patents
Locally power-optimal spacecraft attitude control for redundant reaction wheel clusterSchaub, 2008
View PDF- Document ID
- 3274931805803937552
- Author
- Schaub H
- Publication year
- Publication venue
- AIAA/AAS Astrodynamics Specialist Conference and Exhibit
External Links
Snippet
The attitude control problem of a rigid spacecraft containing a redundant set of reaction wheels is investigated. The classical solution path determines a control solution which requires the smallest set of motor torques. With small micro spacecraft the available power …
- 238000006243 chemical reaction 0 title abstract description 21
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
- B64G1/28—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
- B64G1/26—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
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
- B64G1/24—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
- B64G2001/245—Spacecraft attitude control, e.g. attitude control algorithms
-
- 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
- G05D1/0883—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for space vehicles
-
- 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
- B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
-
- 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 |
---|---|---|
Schaub et al. | Feedback control law for variable speed control moment gyros | |
Leve et al. | Spacecraft momentum control systems | |
Schaub et al. | Redundant reaction wheel torque distribution yielding instantaneous l2 power-optimal spacecraft attitude control | |
Yoon et al. | Adaptive control of uncertain Hamiltonian multi-input multi-output systems: with application to spacecraft control | |
Chesi et al. | Aerodynamic three-axis attitude stabilization of a spacecraft by center-of-mass shifting | |
Hogan et al. | Three-axis attitude control using redundant reaction wheels with continuous momentum dumping | |
US10202208B1 (en) | High control authority variable speed control moment gyroscopes | |
Malladi et al. | Nonlinear model predictive control of coupled rotational-translational spacecraft relative motion | |
Takada et al. | Control moment gyro singularity-avoidance steering control based on singular-surface cost function | |
Blenden et al. | Regenerative power-optimal reaction wheel attitude control | |
Jones et al. | Generalized framework for linearly constrained control moment gyro steering | |
McMahon et al. | Simplified singularity avoidance using variable-speed control moment gyroscope null motion | |
Zavoli et al. | Single-axis pointing of an underactuated spacecraft equipped with two reaction wheels | |
EP1782143A1 (en) | Method and system for optimizing torque in a cmg array | |
Yoon | Spacecraft attitude and power control using variable speed control moment gyros | |
Zidek et al. | Spacecraft drift counteraction optimal control: Open-loop and receding horizon solutions | |
Reijneveld et al. | Attitude control of the Delfi-n3Xt satellite | |
Schaub | Locally power-optimal spacecraft attitude control for redundant reaction wheel cluster | |
Pecora et al. | Robust Attitude Control Using Electrospray Thrusters | |
Agarwal et al. | Inertia-Free Spacecraft Attitude Control with Control Moment Gyroscope Actuation | |
Yoon et al. | Singularity Analysis and Avoidance of Variable-Speed Control Moment Gyros--Part I: No Power Constraint Case | |
Reyhanoglu et al. | Attitude stabilization of a nadir-pointing small satellite using only magnetic actuators | |
Inumoh et al. | Three-axis attitude control of a satellite in zero momentum mode using a tilted wheel methodology | |
DeVon et al. | Closed-Loop Power Tracking for an Integrated Power and Attitude Control System Using Variable-Speed Control Moment Gyroscopes | |
Bedrossian et al. | Space station zero-propellant maneuver guidance trajectories compared to eigenaxis |