Current limiting remote power control module
Abstract
The power source for the Space Station Freedom will be fully utilized nearly all of the time. As such, any loads on the system will need to operate within expected limits. Should any load draw an inordinate amount of power, the bus voltage for the system may sag and disrupt the operation of other loads. To protect the bus and loads some type of power interface between the bus and each load must be provided. This interface is most crucial when load faults occur. A possible system configuration is presented. The proposed interface is the Current Limiting Remote Power Controller (CL-RPC). Such an interface should provide the following power functions: limit overloading and resulting undervoltage; prevent catastrophic failure and still provide for redundancy management within the load; minimize cable heating; and provide accurate current measurement. A functional block diagram of the power processing stage of a CL-RPC is included. There are four functions that drive the circuit design: rate control of current; current sensing; the variable conductance switch (VCS) technology; and the algorithm used for current limiting. Each function is discussed separately.
- Publication:
-
In Alabama Univ
- Pub Date:
- October 1990
- Bibcode:
- 1990asee.nasaR....H
- Keywords:
-
- Algorithms;
- Controllers;
- Electric Potential;
- Heating;
- Loads (Forces);
- Remote Control;
- Space Station Freedom;
- Space Station Power Supplies;
- System Failures;
- Systems Engineering;
- Block Diagrams;
- Disrupting;
- Nasa Programs;
- Redundancy;
- University Program;
- Electronics and Electrical Engineering