Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
Okolo et al., 2020 - Google Patents
[go: Go Back, main page]

Okolo et al., 2020 - Google Patents

Pterodactyl: Development and comparison of control architectures for a mechanically deployed entry vehicle

Okolo et al., 2020

View PDF
Document ID
65436680405109821
Author
Okolo W
Margolis B
D'Souza S
Barton J
Publication year
Publication venue
AIAA SciTech 2020 Forum

External Links

Snippet

The NASA-funded Pterodactyl project seeks to advance the current state-of-the-art for entry vehicles by developing novel guidance and control technologies for Deployable Entry Vehicles (DEVs) that can be applied to various entry vehicle configurations. This paper …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26Guiding or controlling apparatus, e.g. for attitude control using jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/646Docking or rendez-vous systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52Protection, safety or emergency devices; Survival aids
    • B64G1/58Thermal protection, e.g. heat shields
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification

Similar Documents

Publication Publication Date Title
Okolo et al. Pterodactyl: Development and comparison of control architectures for a mechanically deployed entry vehicle
Bhardwaj et al. Integrated reference model for a tilt-rotor vertical take-off and landing transition uav
Adami et al. 6DOF flight control of fixed-wing aircraft by trajectory linearization
Erturk et al. Relative controllability evaluation of mass-actuated airplane
ÇLimen A generic approach to missile autopilot design using state-dependent nonlinear control
Cianciolo et al. Low lift-to-drag morphing shape design
Acosta et al. Adaptive nonlinear dynamic inversion control of an autonomous airship for the exploration of Titan
Johnson et al. Mid-lift-to-drag ratio rigid vehicle control system design and simulation for human mars entry
Varriale et al. A Control Allocation approach to induce the center of pressure position and shape the aircraft transient response
D'Souza et al. Developing an entry guidance and control design capability using flaps for the lifting Nano-ADEPT
Kim et al. Trajectory tracking controller design using neural networks for tiltrotor UAV
Akkinapalli et al. Attitude control of a multicopter using L 1 augmented quaternion based backstepping
Prach et al. Development of a state dependent riccati equation based tracking flight controller for an unmanned aircraft
Restrepo et al. Structured adaptive model inversion controller for Mars atmospheric flight
Mathavaraj et al. Robust control of a reusable launch vehicle in reentry phase using model following neuro-adaptive design
Okolo et al. Development and Evaluation of Control Architectures for a Mechanically Deployed Entry Vehicle
Margolis et al. Control and simulation of a deployable entry vehicle with aerodynamic control surfaces
Dillman et al. Low lift-to-drag morphing shape design
Roenneke et al. Nonlinear flight control for a high-lift reentry vehicle
Gäßler et al. Incremental Nonlinear Dynamic Inversion Flight Control for the DLR Reusability Flight Experiment ReFEx
Hernandez et al. Ascent Flight Control System for Reusable Launch Vehicles: Full Order and Structured H∞ Designs
Artuç et al. Chaotic particle swarm optimisation algorithm based quadrotor control
Brugarolas et al. Entry attitude controller for the Mars Science Laboratory
Sparapany et al. Enabling mars exploration using inflatable Purdue aerodynamic decelerator with deployable entry systems (iPADDLES) technology
Radhakrishnan et al. 6D trajectory, guidance and control development for air-breathing phase of reusable launch vehicle: R. Radhakrishnan et al.