Pages that link to "Item:Q5003567"
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The following pages link to Improved guidance algorithm considering terminal attitude constraints for spacecrafts via optimal control theory (Q5003567):
Displaying 6 items.
- Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission (Q338285) (← links)
- Investigation on single-star stellar-inertial guidance principle using equivalent information compression theory (Q1047373) (← links)
- On high-resolution manoeuvres control via trajectory optimization (Q1692213) (← links)
- A robust and high precision optimal explicit guidance scheme for solid motor propelled launch vehicles with thrust and drag uncertainty (Q2821326) (← links)
- (Q3020686) (← links)
- A Parameter Dependent Spacecraft Guidance Boundary Value Problem (Q5630572) (← links)