Vedantam et al., 2020 - Google Patents
Multi-stage stabilized continuation for indirect optimal control of hypersonic trajectoriesVedantam et al., 2020
View PDF- Document ID
- 16020035383515520583
- Author
- Vedantam M
- Akella M
- Grant M
- Publication year
- Publication venue
- AIAA Scitech 2020 Forum
External Links
Snippet
This work presents the application of stabilized continuation to the planar unpowered hypersonic trajectory generation problem using indirect optimal control methods. This scheme is non-iterative and guaranteed to terminate within a finite number of floating point …
- 239000011159 matrix material 0 description 11
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Vedantam et al. | Multi-stage stabilized continuation for indirect optimal control of hypersonic trajectories | |
Foust et al. | Optimal guidance and control with nonlinear dynamics using sequential convex programming | |
Ozaki et al. | Stochastic differential dynamic programming with unscented transform for low-thrust trajectory design | |
Hu et al. | Robust saturated finite time output feedback attitude stabilization for rigid spacecraft | |
CN104483835B (en) | A kind of flexible spacecraft multiple target integrated control method based on T S fuzzy models | |
Ge et al. | Adaptive neural control of uncertain MIMO nonlinear systems | |
CN112051854B (en) | A fast planning method for optimal trajectory of lunar soft landing considering complex constraints | |
CN103942401A (en) | Tool kit and method for optimizing high-precision self-adaptation and modular spacecraft trajectory multi-constrained track | |
Oguri et al. | Stochastic primer vector for robust low-thrust trajectory design under uncertainty | |
Adurthi et al. | Sparse approximation–based collocation scheme for nonlinear optimal feedback control design | |
Liu et al. | Observer‐based robust adaptive T2 fuzzy tracking control for flexible air‐breathing hypersonic vehicles | |
CN114253291A (en) | Spacecraft formation guidance method and system based on linear pseudo-spectral model predictive control | |
Zuo et al. | Fuzzy adaptive output-feedback constrained trajectory tracking control for HFVs with fixed-time convergence | |
Dearing et al. | Efficient trajectory optimization for constrained spacecraft attitude maneuvers | |
Wu et al. | Introduction to quantitative feedback theory for lateral robust flight control systems design | |
Vedantam et al. | Multistage stabilized continuation for indirect optimal control of three-dimensional hypersonic trajectories | |
Theis | Robust and linear parameter-varying control of aeroservoelastic systems | |
Lee et al. | Time optimal attitude control for a rigid body | |
Tan et al. | Construction of control barrier function and C 2 reference trajectory for constrained attitude maneuvers | |
Wang et al. | Symplectic pseudospectral methods for optimal control: theory and applications in path planning | |
Cui et al. | Finite‐time trajectory tracking control for autonomous airships with uncertainties and external disturbances | |
Biertümpfel et al. | Finite Horizon Worst Case Analysis of Linear Time-Varying Systems Applied to Launch Vehicle | |
Vedantam et al. | Jacobian Conditioned Two-Layer Stabilized Continuation for Computing Optimal Hypersonic Trajectories | |
Liu et al. | Novel prescribed performance control scheme for flexible hypersonic flight vehicles with nonaffine dynamics and neural approximation | |
He et al. | Robust attitude regulation of uncertain spacecraft with flexible appendages |