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#489790
Mon 11 Feb 2019 03:47:PM
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Joined: Feb 2001
Posts: 381,903
Launch Director
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OP
Launch Director
Joined: Feb 2001
Posts: 381,903 |
Abstract: A wealth of literature exists on control allocation algorithms for over-actuated air vehicles, launch vehicles, and spacecraft's. Most of these algorithms focus primarily on minimizing some objective function such as command tracking error and/or control effector usage. Linear allocators (pseudo inverses) are usually the conventional choice due to their simplicity and the ability to achieve a significant portion of the theoretical moment/impulse space. Generally, it is assumed that there exis... Source: An Innovative Control Allocation Scheme to Address Reaction Thruster Interactions on a 3U CubeSat
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An Innovative Control Allocation Scheme to Address Reaction Thruster Interactions on a 3U CubeSat
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Mon 11 Feb 2019 03:47:PM
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