A variational method for multistage launch vehicle optimization
Variational calculus methods used to maximize payload capability for multistage launch vehicles
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Variational calculus methods used to maximize payload capability for multistage launch vehicles
Variational calculus methods for drag reduction of lifting bodies in hypersonic flow
Optimal final value control theory, applying variational calculus and functional analysis to control function selection for dynamic systems
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal control theory of space vehicles
Variational calculus and computer logic for optimization of ascent trajectories and propellant loadings of multistage space vehicles
Sufficient conditions for a weak relative minimum for a form of the Bolza problem of variational calculus are derived. Testing of the second-order conditions requires the backward integration of fewer matrix elements than in the case of most previously published sets of conditions. The derivation is felt to be more complete and straightforward than previous derivations. The variational problem considered is relatively simple, with just a scalar constraint to implicitly or explicitly determine the final time, in order to avoid the complexities associated with controllability considerations. Sufficient conditions for a local minimum for more general optimal control problems can be approached by building upon the derivation and results presented here.
This paper presents a variational formulation of constrained dynamics of flexible multibody systems, using a vector-variational calculus approach. Body reference frames are used to define global position and orientation of individual bodies in the system, located and oriented by position of its origin and Euler parameters, respectively. Small strain linear elastic deformation of individual components, relative to their body references frames, is defined by linear combinations of deformation modes that are induced by constraint reaction forces and normal modes of vibration. A library of kinematic couplings between flexible and/or rigid bodies is defined and analyzed. Variational equations of motion for multibody systems are obtained and reduced to mixed differential-algebraic equations of motion. A space structure that must deform during deployment is analyzed, to illustrate use of the methods developed.
Recent studies have applied variational calculus, conformal mapping, and point transformations to generalize the one-dimensional (1D) space-charge limited current density (SCLCD) and electron emission mechanisms to nonplanar geometries; however, these assessments have focused on extending the Child–Langmuir law (CLL) for SCLCD in vacuum. Since the charge in the diode is independent of the coordinate system (i.e., covariant), we apply bijective point transformations to extend the Mott–Gurney law (MGL) for the SCLCD in a collisional or semiconductor gap to nonplanar 1D geometries. This yields a modified MGL that replaces the Cartesian gap distance with a canonical gap distance that may be written generally in terms of geometric scale factors that are known for multiple geometries. We tabulate results for common geometries. Such an approach may be applied to any current density, including non-space-charge limited gaps and SCLCD that may fall between the CLL and MGL.
Method for first estimate of initial values of Lagrange multipliers for two point boundary value problem of calculus of variations
Differential equations of motion linearized about nominal calculus of variation solution to determine coefficients of guidance function
Maximizing lift-to-drag ratio of slender body in hypersonic flow investigated by calculus of variations
Calculus of variations used to determine minimum time aircraft trajectories between two fixed points in range-altitude space
Minimum drag bodies with elliptical cross section, using Newtonian flow theory and calculus of variations
Optimal smoother derived for linear time-varying systems using measurements containing colored noise by means of calculus of variations
Variational calculus used in obtaining lift drag ratio attainable by slender conical body at hypersonic speeds
Analytical approach to gradient method within framework of Bolza problem of variational calculus, using linearized differential and isoperimetric constraints
Pressurized toroid modified linear membrane theory, presenting approximate solutions for derived boundary value problem by variational calculus methods
The problem of transferring a rocket vehicle from a given circular orbit to a larger coplanar circular orbit in minimum time, using a constant low-thrust rocket engine, is considered. Parameters are chosen to correspond to a transfer from the earth's orbit in heliocentric space to the orbit of Mars. A path satisfying the first order necessary conditions of variational calculus is shown to be locally minimizing by application of a set of second order conditions. A physical explanation is offered to justify the retrothrust period occurring during the flight. A neighboring optimum feedback control law, based on estimated time-to-go, is applied to this problem. State variable and terminal constraint feedback gains are calculated while one of the second order conditions, involving the backward integration of a matrix Riccati equation, is being tested.