刘玥首次大战黑人

HyperPOWER

Hypervelocity Vehicle Controller

HyperPOWER

Hypervelocity vehicles require high-density control systems optimized for size, weight, and power. 刘玥首次大战黑人offers the HyperPOWER controller, which tightly couples actuation and propulsion control, power management, sensor conditioning, and battery activation into a single package. Compared to a classic federated vehicle approach consisting of multiple separate units, a control system based on HyperPOWER provides 25% volume savings and reduced interconnects. HyperPOWER鈥檚 roadmap includes a tactical variant, a space radiation-hardened variant, options to host a flight computer package, and 刘玥首次大战黑人can modify the design for application specific environments and communication protocols.

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Key Features:

  • HyperPOWER integrates actuation, propulsion, and power system control into a single package, yielding increased system performance and savings in volume and latency.
  • A control system based on HyperPOWER offers a single solution to control many aspects of a hypervelocity vehicle, also resulting in reduced programmatic and schedule cost and risk.
  • HyperPOWER includes provisions to incorporate a flight computer for navigation, guidance, attitude, and motion control loops.
  • A robust roadmap drives gated maturation based on relevant testing with HWIL integration and through flight testing.
  • This next generation control system enables increased lethality and range in deployed weapons systems due to reduced weight, power, and volume (25% or greater reduction possible.)

HYPERPOWER 1.0: AEROSPACE GRADE OPTION PERFORMANCE

Characteristics Specifications
Overview 4-channel reconfigurable hypervelocity actuation controller
Power inputs 28 VDC avionics power, 140-270 VDC motor power
Power output Designed for up to 12,000 watts per channel, custom power levels available
Communications RS-422 and LVDS communications
Key features

Sine drive field oriented control, or 6-step motor drive听
Reprogrammable FPGA with external memory and tunable parameters听
Resolver commutation, LVDT feedback interfaces听
Resizable power stages available听
Operation to >1,000 km altitude听

Optional features 4x differential analog telemetry inputs (pressure, temperature, etc.)听
2x squib fire drivers (for battery initiation, pyro initiators, etc.)听
8x solenoid/brake drivers (dual switching)听
Up to 6x additional RTD interfaces听
EEE parts grade Commercial aerospace grade, automotive (AEC-Q-200/100)
Radiation tolerance N/A, technical insertion 鉃 version 2.0 & 3.0
EMI/EMC MIL-STD-461 compliant
Thermals

-40 藲C to +70 藲C baseplate

Physical properties

9.5" x 9.5" x 3.8", 10.5 lbs

Manufacturing IPC-6010 class 3, J-STD-001

HYPERPOWER 2.0: SPACE RADIATION HARDENED OPTION PERFORMANCE

Characteristics Specifications
Overview 2-4-channel reconfigurable space radiation hardened hypervelocity actuation controller
Power inputs 28 VDC avionics power, 140-270 VDC motor power
Power output Designed for up to 12,000 watts per channel, custom power levels available
Communications RS-422 and discrete digital safety/interlock interfaces
Key features

Qty 2 or qty 4 sine drive field oriented control or 6-step motor drive
Qty 6 solenoid drivers for ACS thrusters
Reprogrammable FPGA with external memory and tunable parameters
Resolver commutation, LVDT feedback interfaces
Resizable power stages available
Space radiation hardened logic/ACS electronics for operation through exo-atmospheric flight

Optional features 4x differential additional analog telemetry (pressure, temperature)
2x squib fire drivers (for battery initiation, pyro initiators, etc.)
2x additional solenoid drivers (brake drive, pin-pullers, etc.)
Up to 6x additional RTD interfaces听
EEE parts grade Control/ACS electronics: space radiation hardened
Power electronics: Commercial aerospace grade, PEMS/automotive (AEC-Q-200/100), powered off during exoatmospheric flight
EMI/EMC MIL-STD-461 compliant
Thermals

40 藲C to +70 藲C baseplate

Physical properties

2-channel variant: 9.5鈥 x 6.5鈥 x 3.8鈥, 10.0 lb

Manufacturing IPC-6010 class 3, J-STD-001