This paper develops a fault tolerant attitude controller for next generation nanostatellites
A robust control allocation scheme is developed for rigid spacecraft attitude stabilization in the p...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
This paper develops a fault-tolerant attitude controller for next-generation nanosatellites. The pro...
This paper documents the development and testing of a fault tolerant sliding mode attitude control a...
Since nano-spacecraft are small, low cost and do not undergo the same rigor of testing as convention...
Since nano-spacecraft are small, low cost and do not undergo the same rigor of testing as convention...
While nonlinear attitude control has been explored widely in theory, nanosatellite air-bearing-based...
Abstract: New results on methods and software for nonlinear dynamic research and design of robust gy...
In this paper, a decentralized fault-tolerant control (FTC) system is proposed for near-space vehicl...
The analysis, verification and emulation of attitude control hardware for nanosatellite spacecraft i...
Nano-satellites are classified as satellites weighing less than 20kg. This dissertation presents ...
students to design and build satellites. The mission requires an attitude determination and control ...
none3This paper explains the design method of an innovative active fault tolerant control scheme and...
The paper addresses the problem of fault tolerant control design that has the same effect as implici...
A robust control allocation scheme is developed for rigid spacecraft attitude stabilization in the p...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
This paper develops a fault-tolerant attitude controller for next-generation nanosatellites. The pro...
This paper documents the development and testing of a fault tolerant sliding mode attitude control a...
Since nano-spacecraft are small, low cost and do not undergo the same rigor of testing as convention...
Since nano-spacecraft are small, low cost and do not undergo the same rigor of testing as convention...
While nonlinear attitude control has been explored widely in theory, nanosatellite air-bearing-based...
Abstract: New results on methods and software for nonlinear dynamic research and design of robust gy...
In this paper, a decentralized fault-tolerant control (FTC) system is proposed for near-space vehicl...
The analysis, verification and emulation of attitude control hardware for nanosatellite spacecraft i...
Nano-satellites are classified as satellites weighing less than 20kg. This dissertation presents ...
students to design and build satellites. The mission requires an attitude determination and control ...
none3This paper explains the design method of an innovative active fault tolerant control scheme and...
The paper addresses the problem of fault tolerant control design that has the same effect as implici...
A robust control allocation scheme is developed for rigid spacecraft attitude stabilization in the p...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
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