Closed-loop control algorithm architecture. Through real-time state feedback from high-frequency sensors and a multi-channel redundant computing architecture, it ensures command execution and flight attitude control achieve a real-time, high-precision closed loop at the sub-millisecond level.
Redundant sensors capture high-precision proactive flight commands and perform first-stage intelligent voting on air data and inertial navigation attitude information.
The core flight control computer runs high-frequency closed-loop algorithms, performing fault-tolerant solving via hard real-time redundancy logic to precisely compute current deviation control laws.
Intelligent actuation controllers allocate control power with millisecond-level rapid response, adjusting control surfaces and thrust vectors to complete attitude deflection control.
High-frequency sensor arrays accurately capture current attitude angular velocities, g-loads, and surface states, seamlessly returning deviations to the input stage for the next iteration.