The reliability of static space nuclear power systems (SNPSs) could be impr
oved through the use of backup devices in addition to shunt regulators, as
currently proposed for load following. Shunt regulator failure leading to r
eactor shutdown is possible, as is the possible need to deliver somewhat hi
gher power level to the load than originally expected. A backup system is p
roposed in SNPSs to eliminate the possibility of a single-point failure in
the shunt regulators and to increase the overall system power delivery capa
bility despite changing mission needs and component characteristics. The ob
jective of this paper is to demonstrate the feasibility of such a backup de
vice for voltage regulation in static SNPSs that is capable of overcoming s
ystem variations resulting from operation at different power levels. A dyna
mic compensator is designed using the Linear Quadratic Gaussian with Loop T
ransfer Recovery method. The resulting compensators are gain scheduled usin
g the SNPS electric power as the scheduling variable, resulting in a nonlin
ear compensator. The performance of the gain-scheduled compensator is inves
tigated extensively using an SNPS simulator. The simulations demonstrate th
e effects of the fuel temperature reactivity coefficient variations on the
load-following capabilities of the SNPS, Robustness analysis results demons
trate that the proposed controller exhibits significant operational flexibi
lity, and it can be considered for long-term space mission requiring signif
icant levels of autonomy.